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<article article-type="research-article" dtd-version="3.0" xml:lang="en" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink">
	<front>
		<journal-meta>
			<journal-id journal-id-type="publisher-id">MC</journal-id>
			<journal-title-group>
				<journal-title>Materiales de Construcci&#x00F3;n</journal-title>
			</journal-title-group>
			<issn pub-type="epub">0465-2746</issn>
			<publisher>
				<publisher-name>Consejo Superior de Investigaciones Cientificas</publisher-name>
			</publisher>
		</journal-meta>
		<article-meta>
			<article-id pub-id-type="publisher-id">MC201310-e007-01513</article-id>
			<article-id pub-id-type="doi">10.3989/mc.2014.01513</article-id>
			<article-categories>
				<subj-group subj-group-type="heading">
					<subject>Articles</subject>
				</subj-group>
			</article-categories>
			<title-group>
				<article-title>Experimental study of masonry wall exposed to blast loading</article-title>
				<trans-title-group xml:lang="es">
					<trans-title>Estudio experimental del comportamiento de una f&#x00E1;brica sometida a cargas explosivas</trans-title>
				</trans-title-group>
				<alt-title alt-title-type="running-head">Experimental study of masonry wall exposed to blast loading</alt-title>
			</title-group>
			<contrib-group>
				<contrib contrib-type="author">
					<name>
						<surname>Ahmad</surname>
						<given-names>S.</given-names>
					</name>
					<xref ref-type="aff" rid="AF0001">a</xref>
				</contrib>
				<contrib contrib-type="author">
					<name>
						<surname>Elahi</surname>
						<given-names>A.</given-names>
					</name>
					<xref ref-type="aff" rid="AF0001">a</xref>
				</contrib>
				<contrib contrib-type="author">
					<name>
						<surname>Pervaiz</surname>
						<given-names>H.</given-names>
					</name>
					<xref ref-type="aff" rid="AF0001">a</xref>
				</contrib>
				<contrib contrib-type="author">
					<name>
						<surname>Rahman</surname>
						<given-names>A.G.A.</given-names>
					</name>
					<xref ref-type="aff" rid="AF0002">b</xref>
				</contrib>
				<contrib contrib-type="author" corresp="yes">
					<name>
						<surname>Barbhuiya</surname>
						<given-names>S.</given-names>
					</name>
					<xref ref-type="aff" rid="AF0003">c</xref>
					<xref ref-type="corresp" rid="cor1">&#x002A;</xref>
				</contrib>
			</contrib-group>
			<aff id="AF0001">
				<label>a</label>University of Engineering and Technology (Taxila, Pakistan)</aff>
			<aff id="AF0002">
				<label>b</label>University of Malaysia (Pahang, Malaysia)</aff>
			<aff id="AF0003">
				<label>c</label>Curtin University of Technology (Perth, Australia)</aff>
			<author-notes>
				<corresp id="cor1">
					<label>&#x002A;</label>
					<email xlink:href="Salim.Barbhuiya@curtin.edu.au">Salim.Barbhuiya@curtin.edu.au</email>
				</corresp>
			</author-notes>
			<pub-date pub-type="epub">
				<day>31</day>
				<month>03</month>
				<year>2014</year>
			</pub-date>
			<pub-date pub-type="collection">
				<year>2014</year>
			</pub-date>
			<volume>64</volume>
			<issue>313</issue>
			<elocation-id content-type="doi">10.3989/mc.2014.01513</elocation-id>
			<history>
				<date date-type="received">
					<day>13</day>
					<month>02</month>
					<year>2013</year>
				</date>
				<date date-type="accepted">
					<day>10</day>
					<month>07</month>
					<year>2013</year>
				</date>
				<date date-type="Available on line">
					<day>18</day>
					<month>03</month>
					<year>2014</year>
				</date>
			</history>
			<permissions>
				<copyright-statement>&#x00A9; 2014 CSIC</copyright-statement>
				<copyright-year>2014</copyright-year>
				<license license-type="open-access" xlink:href="http://creativecommons.org/licenses/by-nc/3.0/">
					<license-p>This is an open-access article distributed under the terms of the Creative Commons Attribution-Non Commercial (by-nc) Spain 3.0 License.</license-p>
				</license>
			</permissions>
			<abstract>
				<title>ABSTRACT</title>
				<p>The challenge of protecting the nation against the attack of terrorism has raised the importance to explore the understanding of building materials against the explosion. Unlike most of the building materials, brick masonry materials offer relatively small resistance against blast loading. In this research, a brick masonry wall was exposed to varying blast load at different scaled distances. Six tests with different amounts of explosives at various distances were carried out. Pressure time history, acceleration time history and strain at specific location were measured. The parameters measured from experimental pressure time history and acceleration time history is compared with those determined by ConWep to establish the correlations between experimental determined records and ConWep values. The experimental results were also compared with some researchers. These correlations may assist in understanding the behaviour of masonry structures subjected to explosive loading.</p>
			</abstract>
			<trans-abstract xml:lang="es">
				<title>RESUMEN</title>
				<p>
					<italic>Estudio experimental del comportamiento de una f&#x00E1;brica sometida a cargas explosivas.-</italic> Con el reto que supone proteger a la naci&#x00F3;n contra atentados terroristas se ha visto acrecentada la importancia de conocer el comportamiento de materiales de construcci&#x00F3;n cuando se someten a una carga explosiva. Al contrario de la mayor&#x00ED;a de los materiales, las f&#x00E1;bricas de ladrillo ofrecen poca resistencia a dichas cargas. En el presente trabajo, se estudi&#x00F3; el comportamiento de una f&#x00E1;brica de ladrillo ante cargas explosivas colocadas a diferentes distancias del muro. Se realizaron seis pruebas con explosivos de potencias distintas y a diferentes distancias. Se trazaron las curvas presi&#x00F3;n-tiempo y aceleraci&#x00F3;n-tiempo, midi&#x00E9;ndose asimismo la deformaci&#x00F3;n en un punto concreto. Los valores experimentales de las curvas presi&#x00F3;n-tiempo y aceleraci&#x00F3;n-tiempo se compararon con los que se calcularon con la ayuda de la aplicaci&#x00F3;n inform&#x00E1;tica ConWep a fin de establecer las correlaciones entre ambos conjuntos de resultados. Tambi&#x00E9;n se compararon los resultados experimentales obtenidos con los publicados por otros investigadores. Estas correlaciones podr&#x00ED;an contribuir a mejorar el conocimiento del comportamiento de estructuras de f&#x00E1;brica sometidas a cargas explosivas.</p>
			</trans-abstract>
			<kwd-group xml:lang="en">
				<title>KEYWORDS</title>
				<kwd>Brick</kwd>
				<kwd>Acceleration</kwd>
				<kwd>Deformation</kwd>
				<kwd>Compressive strength</kwd>
			</kwd-group>
			<kwd-group xml:lang="es">
				<title>PALABRAS CLAVE</title>
				<kwd>Ladrillo</kwd>
				<kwd>Aceleraci&#x00F3;n</kwd>
				<kwd>Deformaci&#x00F3;n</kwd>
				<kwd>Resistencia a la compresi&#x00F3;n</kwd>
			</kwd-group>
		</article-meta>
	</front>
	<body>
		<sec id="S0001">
			<title>1. INTRODUCTION</title>
			<p>The threat of terrorism has increased the need for engineers to have confidence that buildings can withstand the significant loads experienced during a blast event. The destruction of load bearing masonry walls can lead to the more serious problem of progressive collapse, it is therefore important that behaviour of masonry structure must be known in order to take special measures to avoid structural failure. Masonry walls are generally used in almost all types of building construction in different parts of the world and have considerable historical and architectural worth. Masonry walls have many advantages such as easy availability, low cost building material, and excellent sound and insulation properties. Under blast loading, masonry walls exhibit brittle behaviour. Failure of a masonry wall is likely to be sudden and severe that pose significant debris hazard to building occupants when subjected to blast loads (<xref ref-type="bibr" rid="CIT0001">1</xref>, <xref ref-type="bibr" rid="CIT0002">2</xref>). Based on field test observations, the damages on the wall were classified in four levels by Varma et al. (<xref ref-type="bibr" rid="CIT0003">3</xref>). Blast explosions generate pressures of high intensity and short duration. These extreme forces cause enormous displacement deformation and the resulting breakage of nearby objects. The term of explosion means a large scale, sudden and rapid release of the energy in an extreme manner followed by pressure wave propagation. The mutual interactions of the air and obstacles at the interface will decide the structural response, damage and fracture. Retrofitting of wall is a practical way of reducing the susceptibility to blast loading, thereby, mitigating danger to occupants in the occurrence of an external explosion (<xref ref-type="bibr" rid="CIT0001">1</xref>). Different studies have raised different parameters to strengthen masonry wall against such an extreme loading cases (<xref ref-type="bibr" rid="CIT0004">4</xref>, <xref ref-type="bibr" rid="CIT0005">5</xref>). The pressure impulse curves defining different damage areas have been extensively used for assessing the damage of masonry walls and other structural components subjected to blast loads (<xref ref-type="bibr" rid="CIT0006">6</xref>).</p>
			<p>Behavior of structures when subjected to both air blast and ground shock pressure waves from surface explosion were studied by Wu &#x0026; Hao (<xref ref-type="bibr" rid="CIT0007">7</xref>). One story masonry in-filled reinforced concrete frame was considered in the investigation. Dynamic response of the structures to the pressure forces was then calculated. It was concluded that air blast load dominates structural response and damage for small scaled distances, whereas, ground shock pressure governs surface explosion at large scaled distance. Also it was investigated that at large scaled distance, ground shock and air blast force can be evaluated separately as the effects of both on structures decoupled. It was further concluded that structural damage would be seriously underestimated if ground shock were neglected under certain conditions. Godinho et al. (<xref ref-type="bibr" rid="CIT0008">8</xref>) studied resistance of unreinforced masonry walls to air blast loads. Authors demonstrated that the wall would have undergone out-of-plane flexure and produced tensile strains on the inner face of the wall and compressive strains on the exterior face when encountered to an air blast load. The wall, then would have gone through negative deflection developing tensile strains on the exterior face of the wall and amplifying shear stresses at wall supports. So it was suggested that exterior masonry walls should be made stronger with glazed elements. As the breakage of these elements release some blast pressure, this reduces the effect of blast load forces on the remaining structure.</p>
			<p>Analysis and design of structures under blast explosion require a detail understanding of blast phenomenon and dynamic response of structural elements. Ngo et al. (<xref ref-type="bibr" rid="CIT0009">9</xref>) discussed nature of explosions, blast wave propagation in air and different techniques used to predict the response of structure when detonated. It was highly recommended to use technical design manuals in current building design codes to prevent structure vulnerability and progressive collapse. Urgessa (<xref ref-type="bibr" rid="CIT0010">10</xref>) conducted a blast test on eight masonry walls retrofitted with fibre reinforced polymer. These walls were exposed to blast loads of 0.45 kg. Pressure time history and displacement response of the structure were measured. Measured blast wave parameters were observed to be in a good agreement with parameters determined from Single-Degree-of-Freedom (SDOF) dynamic analysis.</p>
			<p>In another study, numerical simulations on LS DYNA were carried out for the assessment of the response of unreinforced brick masonry walls exposed to blast loading (<xref ref-type="bibr" rid="CIT0011">11</xref>). The effects of material strength, boundary conditions and thickness of the wall under blast loads were studied. It was concluded that there was a marginal effect of mortar and brick strength on the structural response under larger detonation. Thickness of the wall was observed to be a dominating parameter in producing considerable effect on the response and damage of masonry walls. Different types of boundary conditions of the wall were taken into consideration. It was found that the boundary condition has a remarkable effect on the response and failure of the walls.</p>
			<p>In a recent study, effect of variety of commonly used material was examined from existing literature on blast loading (<xref ref-type="bibr" rid="CIT0012">12</xref>). This study is an important tool to blast investigators in order to understand the effect of size and location of the blast explosive from the target. Five conventional buildings were reviewed in terms of observed damage on the material after blasting. Most of the research has been undertaken in the field of dynamic analysis for the modeling of blast pressure on the structures (<xref ref-type="bibr" rid="CIT0013">13</xref>&#x2013;<xref ref-type="bibr" rid="CIT0015">15</xref>). The present results allow a detailed study of the simultaneous air blast pressure and ground shock on structures. Unreinforced masonry walls are commonly susceptible to out-of-plane loads. It is, thus, of interest to understand the behavior of unreinforced masonry walls under blast loading. The current research work will contribute in understanding the behaviour of masonry wall against explosion loads.</p>
		</sec>
		<sec id="S0002">
			<title>2. EXPERIMENTAL PROGRAMME</title>
			<sec id="S20003">
				<title>2.1. Experimental Scheme</title>
				<p>A masonry wall of 2 m&#x00D7;2 m was constructed. A scheme of wall is shown in <xref ref-type="fig" rid="F0001">Figure 1</xref>. The wall was then exposed to varying blast loads. Six tests with different amounts of explosives were carried out. Quantity of charge was varied from 4 kg to 14 kg with an increment of 2 kg. Distance of explosive location to the target centre varies from 3 m to 4 m respectively. Nitroglycerin based dynamite explosive was used. Vertical wooden support was erected to hold charge mass 1m above the ground. This whole work had been carried out in hilly area of Hassan-Abdal (Punjab), Pakistan. TNT equivalent of nitroglycerin dynamite explosive is 0.6. It is customary to refer the weight of explosives used in experimental tests to an equivalent weight of TNT. Formby &#x0026; Wharton (<xref ref-type="bibr" rid="CIT0016">16</xref>) offered results to obtain TNT equivalency of various commercial explosives. Material properties of brick are given in <xref ref-type="table" rid="T0001">Table 1</xref>. Experimental data of six tests with different standoff distance and amount of explosive used is given in <xref ref-type="table" rid="T0002">Table 2</xref>.
</p>
				<fig id="F0001">
					<label>Figure 1</label>
					<caption>
						<p>View of brick masonry wall.</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g001.tif"/>
				</fig>
				<table-wrap id="T0001">
					<label>Table 1</label>
					<caption>
						<p>Material properties of brick</p>
					</caption>
					<table frame="hsides" rules="groups">
						<thead>
							<tr>
								<th align="left">Constructive element</th>
								<th align="center">Density &#x3C1; (kg/m<sup>3</sup>)</th>
								<th align="center">Compressive strength f<sub>c</sub> (MPa)</th>
								<th align="center">Young&#x2019;s Modulus E (MPa)</th>
								<th align="center">Poisson&#x2019;s ratio &#x3BD;</th>
							</tr>
						</thead>
						<tbody>
							<tr>
								<td align="left">Solid clay brick</td>
								<td align="center">1800</td>
								<td align="center">6.76</td>
								<td align="center">6084</td>
								<td align="center">0.17</td>
							</tr>
						</tbody>
					</table>
				</table-wrap>
				<table-wrap id="T0002">
					<label>Table 2</label>
					<caption>
						<p>Experimental data</p>
					</caption>
					<table frame="hsides" rules="groups">
						<thead>
							<tr>
								<th align="center" colspan="4">BRICK MASONRY WALL (2m&#xD7;2m&#xD7;0.381m)</th>
							</tr>
							<tr>
								<th align="center" colspan="4"><hr/></th>
							</tr>
							<tr>
								<th align="left">Charge mass, Q (kg)</th>
								<th align="center">TNT Equivalent Weight, Q<sub>TNT</sub>(kg)</th>
								<th align="center">Stand-off distance, R (m)</th>
								<th align="center">Scaled distance Z = R/Q<sup>1/3</sup> [m/(kg<sup>1/3</sup>)]
								</th>
							</tr>
						</thead>
						<tbody>
							<tr>
								<td align="left">4</td>
								<td align="center">2.4</td>
								<td align="center">3</td>
								<td align="center">2.24</td>
							</tr>
							<tr>
								<td align="left">6</td>
								<td align="center">3.6</td>
								<td align="center">3.5</td>
								<td align="center">2.28</td>
							</tr>
							<tr>
								<td align="left">8</td>
								<td align="center">4.8</td>
								<td align="center">3.5</td>
								<td align="center">2.07</td>
							</tr>
							<tr>
								<td align="left">10</td>
								<td align="center">6</td>
								<td align="center">4</td>
								<td align="center">2.20</td>
							</tr>
							<tr>
								<td align="left">12</td>
								<td align="center">7.2</td>
								<td align="center">3.5</td>
								<td align="center">1.81</td>
							</tr>
							<tr>
								<td align="left">14</td>
								<td align="center">8.4</td>
								<td align="center">3.5</td>
								<td align="center">1.72</td>
							</tr>
						</tbody>
					</table>
				</table-wrap>
			</sec>
			<sec id="S20004">
				<title>2.2. Measuring devices and explosive charge</title>
				<p>Different measuring instruments were installed to record pressure, acceleration and strains at a given locations over time during the test. Measurement devices give strain, pressure time history and acceleration time history; an important element concerning response of structures to air blast loading. These parameters were measured using pressure sensors, accelerometer and data acquisition system. For better understanding of the complex dynamic response, high-speed camera was used. Different measuring devices were employed to monitor the response of masonry wall to the blast loading. PCB Sensors of 200 psi range was used in current blast wall pressure measurement to measure the overpressure generated by shock waves. This sensor was placed at the center of the wall exposed to impulsive loading as shown in <xref ref-type="fig" rid="F0002">Figure 2</xref>. PCB pressure sensor is Integrated-Circuit Piezoelectric (ICP) voltage mode sensor. This converts input pressure to high-resolution curve that is virtually insensitive to length of cable. It was connected to the data acquisition system module shown in <xref ref-type="fig" rid="F0002">Figure 2</xref>.</p>
				<fig id="F0002">
					<label>Figure 2</label>
					<caption>
						<p>Scheme of Pressure sensor.</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g002.tif"/>
				</fig>
				<p>In order to measure dynamic response of wall in three mutually perpendicular axes, triaxial accelerometer was used in blasting on brick masonry wall. It was fixed at the center and on backside of concrete wall using adhesive as shown in <xref ref-type="fig" rid="F0003">Figure 3</xref>. After preparation of the surface, the strain gauges were glued at the centre of the masonry wall as shown in the <xref ref-type="fig" rid="F0004">Figure 4</xref>. Strain gauges were connected to Strain Indicator and Recorder. It has four input channels. LCD display of the equipment readout the strain.</p>
				<fig id="F0003">
					<label>Figure 3</label>
					<caption>
						<p>Location of Accelerometer (Backside of wall).</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g003.tif"/>
				</fig>
				<fig id="F0004">
					<label>Figure 4</label>
					<caption>
						<p>Location for strain gauge installation.</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g004.tif"/>
				</fig>
				<p>In addition a data acquisition instruments was used. It was mounted on a computer that record and process the signals by means of a computer program. It has 16 input channels, 2 output channels and has a capacity of 200 KS/s (Kilo Sample/Second) and16-bit Multifunction I/O. Nitroglycerin Based Dynamites was used in this experiment of blasting operation. In this test, it is used in 80% in mass of TNT. Images of blast explosion captured by high-speed camera are shown in <xref ref-type="fig" rid="F0005">Figure 5</xref>.</p>
				<fig id="F0005">
					<label>Figure 5</label>
					<caption>
						<p>High-speed camera images of blast wave propagation.</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g005.tif"/>
				</fig>
				<p>
					<xref ref-type="fig" rid="F0006">Figure 6</xref> shows the damage pattern of detonated masonry wall. It can be noted that when the quantity of explosive was 6 kg, insignificant cracks were observed. Masonry wall still maintains the integrity as before. With the increase in the quantity of the explosive, several cracks along the longitudinal direction were noticed. Depth of cracks grows with increasing the quantity of explosive. Under the explosive load of 12 kg, a large longitudinal crack along the front and back side of the wall was noticed. It was observed that masonry wall suffered from a non-repairable damage. For 14 kg explosive load, the wall fall down along the weak plane i.e. along longitudinal crack.</p>
				<fig id="F0006">
					<label>Figure 6</label>
					<caption>
						<p>Blast loaded wall after explosion.</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g006.tif"/>
				</fig>
			</sec>
		</sec>
		<sec id="S0005">
			<title>3. RESULTS AND DISCUSSION</title>
			<p>The brick wall collapsed in the field at 14 kg explosive load. The results from all six tests are presented below:</p>
			<sec id="S20006">
				<title>3.1. Pressure time history</title>
				<p>Records of the time histories of the overpressure that was measured at the centre of brick wall are shown in <xref ref-type="fig" rid="F0007">Figures 7</xref> and <xref ref-type="fig" rid="F0008">8</xref>. Pressure wave follows the classical shape of pressure time history.</p>
				<fig id="F0007">
					<label>Figure 7</label>
					<caption>
						<p>Measured pressure-time history of 10 kg surface explosion (4 m from charge centre).</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g007.tif"/>
				</fig>
				<fig id="F0008">
					<label>Figure 8</label>
					<caption>
						<p>Measured pressure-time history of 12 kg surface explosion (3.5 m from charge centre).</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g008.tif"/>
				</fig>
			</sec>
			<sec id="S20007">
				<title>3.2. Acceleration time history</title>
				<p>The accelerations that were measured in all three directions at the centre of the wall are shown in <xref ref-type="fig" rid="F0009">Figures 9</xref> and <xref ref-type="fig" rid="F0010">10</xref>. The obtained value of acceleration has a connection with the damage/failure pattern of the specimen.</p>
				<fig id="F0009">
					<label>Figure 9</label>
					<caption>
						<p>Acceleration time history (g<sub>x</sub>) of 10 kg surface explosion (4 m from charge centre).</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g009.tif"/>
				</fig>
				<fig id="F0010">
					<label>Figure 10</label>
					<caption>
						<p>Acceleration time history (g<sub>y</sub>) of 10 kg surface explosion, 4 m from charge centre.</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g010.tif"/>
				</fig>
			</sec>
			<sec id="S20008">
				<title>3.3. Experimental results of strain</title>
				<p>The time dependent strains that were measured at the center of the brick wall are shown in <xref ref-type="fig" rid="F0011">Figure 11</xref>. 45&#x00B0; strain rosette was used. It is clearly seen that peak strain for 12 kg explosion was greater than six explosive loads.</p>
				<fig id="F0011">
					<label>Figure 11</label>
					<caption>
						<p>Strain vs. time of brick wall under explosive load.</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g011.tif"/>
				</fig>
			</sec>
			<sec id="S20009">
				<title>3.4. Comparison with predicted values</title>
				<p>Comparison of calculated parameters with ConWep (<xref ref-type="bibr" rid="CIT0017">17</xref>) is done to check correlation between experimental determined records and ConWep values. The present results allow a detailed study of the simultaneous airblast pressure and ground shock on structures.</p>
				<sec>
					<title>3.4.1. Air blast wave parameters</title>
					<p>Usually the air blast wave parameters are peak pressure P<sub>so</sub>, arrival time T<sub>a</sub>, rising time to the peak value of pressure T<sub>r</sub> and decreasing time from peak to ambient pressure T<sub>d</sub> and total duration of positive pressure phase of pressure time history are given in <xref ref-type="table" rid="T0003">Table 3</xref>.
</p>
					<table-wrap id="T0003">
						<label>Table 3</label>
						<caption>
							<p>Experimental values of air blast wave parameters</p>
						</caption>
						<table frame="hsides" rules="groups">
							<thead>
								<tr>
									<th align="center"/>
									<th align="center" colspan="6">AIR BLAST WAVE PARAMETERS</th>
								</tr>
								<tr>
									<th align="center"/>
									<th align="left" colspan="6"><hr/></th>
								</tr>
								<tr>
									<th align="left" rowspan="3" valign="bottom">Scaled distance (m/kg<sup>1/3</sup>)</th>
									<th align="center" colspan="2">P<sub>so</sub> (MPa)</th>
									<th align="center"/>
									<th align="center"/>
									<th align="center"/>
									<th align="center"/>
								</tr>
								<tr>
									<th align="left" colspan="2"><hr/></th>
									<th align="center"/>
									<th align="center"/>
									<th align="center"/>
									<th align="center"/>
									<th align="center"/>
								</tr>
								<tr>
									<th align="center">Experimental</th>
									<th align="center">TM-5</th>
									<th align="center">T<sub>a</sub> (sec)</th>
									<th align="center">T<sub>r</sub> (sec)</th>
									<th align="center">T<sub>d</sub> (sec)</th>
									<th align="center">T (sec)</th>
								</tr>
							</thead>
							<tbody>
								<tr>
									<td align="left">1.72</td>
									<td align="center">0.6115</td>
									<td align="center">0.5502</td>
									<td align="center">0.01301</td>
									<td align="center">0.00088</td>
									<td align="center">0.00179</td>
									<td align="center">0.00267</td>
								</tr>
								<tr>
									<td align="left">1.81</td>
									<td align="center">0.4099</td>
									<td align="center">0.4791</td>
									<td align="center">0.0159</td>
									<td align="center">0.00067</td>
									<td align="center">0.00173</td>
									<td align="center">0.0024</td>
								</tr>
								<tr>
									<td align="left">2.07</td>
									<td align="center">0.2776</td>
									<td align="center">0.339</td>
									<td align="center">0.012</td>
									<td align="center">0.00155</td>
									<td align="center">0.0022</td>
									<td align="center">0.00375</td>
								</tr>
								<tr>
									<td align="left">2.20</td>
									<td align="center">0.2692</td>
									<td align="center">0.3357</td>
									<td align="center">0.01298</td>
									<td align="center">0.00114</td>
									<td align="center">0.00253</td>
									<td align="center">0.00367</td>
								</tr>
								<tr>
									<td align="left">2.24</td>
									<td align="center">0.2158</td>
									<td align="center">0.2654</td>
									<td align="center">0.01099</td>
									<td align="center">0.00052</td>
									<td align="center">0.003115</td>
									<td align="center">0.00364</td>
								</tr>
								<tr>
									<td align="left">2.28</td>
									<td align="center">0.2075</td>
									<td align="center">0.275</td>
									<td align="center">0.01</td>
									<td align="center">0.00049</td>
									<td align="center">0.00331</td>
									<td align="center">0.0038</td>
								</tr>
							</tbody>
						</table>
					</table-wrap>
				</sec>
				<sec>
					<title>3.4.2. Peak air pressure</title>
					<p>Using the experimental pressure time history, the peak value of incident overpressure is determined. Comparison between peak values of pressure determined by experimental pressure time data, ConWep calculated values, UFC (<xref ref-type="bibr" rid="CIT0018">18</xref>) and AASTP (<xref ref-type="bibr" rid="CIT0019">19</xref>) for hemispherical surface explosion along with their best fitted curve are reported in <xref ref-type="table" rid="T0004">Table 4</xref> and are further graphically shown in <xref ref-type="fig" rid="F0012">Figure 12</xref>. As shown, the experimental variation of peak pressure with scaled distance confirmed the results calculated by means of ConWep, UFC and AASTP chart for hemispherical surface explosion. Experimental results are comparatively more consistent with those as predicted by AASTP.
</p>
					<fig id="F0012">
						<label>Figure 12</label>
						<caption>
							<p>Relationship between peak pressure attenuation and standoff distances.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g012.tif"/>
					</fig>
					<table-wrap id="T0004">
						<label>Table 4</label>
						<caption>
							<p>Comparison of experimental peak pressure with ConWep and other published work</p>
						</caption>
						<table frame="hsides" rules="groups">
							<thead>
								<tr>
									<th align="left" rowspan="3" valign="bottom">Scaled distance (m/kg<sup>1/3</sup>)</th>
									<th align="center" colspan="4">P<sub>so</sub>(MPa)</th>
								</tr>
								<tr>
									<th align="center" colspan="4"><hr/></th>
								</tr>
								
								<tr>
									<th align="center">Experimental</th>
									<th align="center">ConWep</th>
									<th align="center">UFC</th>
									<th align="center">AASTP</th>
								</tr>
							</thead>
							<tbody>
								<tr>
									<td align="left">1.72</td>
									<td align="center">0.6115</td>
									<td align="center">0.489612</td>
									<td align="center">0.5502</td>
									<td align="center">0.57</td>
								</tr>
								<tr>
									<td align="left">1.81</td>
									<td align="center">0.4099</td>
									<td align="center">0.432874</td>
									<td align="center">0.4791</td>
									<td align="center">0.43</td>
								</tr>
								<tr>
									<td align="left">2.07</td>
									<td align="center">0.2776</td>
									<td align="center">0.31285</td>
									<td align="center">0.339</td>
									<td align="center">0.258</td>
								</tr>
								<tr>
									<td align="left">2.20</td>
									<td align="center">0.2692</td>
									<td align="center">0.277346</td>
									<td align="center">0.3357</td>
									<td align="center">0.224</td>
								</tr>
								<tr>
									<td align="left">2.24</td>
									<td align="center">0.2158</td>
									<td align="center">0.251838</td>
									<td align="center">0.2654</td>
									<td align="center">0.216</td>
								</tr>
								<tr>
									<td align="left">2.28</td>
									<td align="center">0.2075</td>
									<td align="center">0.248598</td>
									<td align="center">0.275</td>
									<td align="center">0.2062</td>
								</tr>
							</tbody>
						</table>
					</table-wrap>
				</sec>
				<sec>
					<title>3.4.3. Comparison between empirical equations of P<sub>so</sub></title>
					<p>Many empirical relationships are available in the literature for predicting peak overpressure attenuation against scaled ranges. Brode&#x2019;s (<xref ref-type="bibr" rid="CIT0013">13</xref>, <xref ref-type="bibr" rid="CIT0020">20</xref>, <xref ref-type="bibr" rid="CIT0021">21</xref>) empirical formulae for peak pressure in an unlimited atmosphere are [<xref ref-type="disp-formula" rid="FD1">1</xref>] [<xref ref-type="disp-formula" rid="FD2">2</xref>]:<disp-formula id="FD1">
							<alternatives>
								<mml:math id="M1">
									<mml:mrow>
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											<mml:mi>p</mml:mi>
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												<mml:mi>o</mml:mi>
											</mml:mrow>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mn>0.67</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
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								<mml:math id="M2">
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								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq002.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<p>Wu nd Hao (<xref ref-type="bibr" rid="CIT0022">22</xref>) determined peak pressure at the target points in the air using simulated pressure time histories at a hemispherical shock wave front is [<xref ref-type="disp-formula" rid="FD3">3</xref>]:<disp-formula id="FD3">
							<alternatives>
								<mml:math id="M3">
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										<mml:mn>0.059</mml:mn>
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																			<mml:mn>1</mml:mn>
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																			<mml:mn>3</mml:mn>
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														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>2.56</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo>-</mml:mo>
										<mml:mn>0.051</mml:mn>
										<mml:mo>,</mml:mo>
										<mml:mtext>0.1</mml:mtext>
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											<mml:mrow>
												<mml:mn>1</mml:mn>
												<mml:mo>/</mml:mo>
												<mml:mn>3</mml:mn>
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										<mml:mo>&#x2264;</mml:mo>
										<mml:mn>1</mml:mn>
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										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq003.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<p>Siddiqui and Ahmad (<xref ref-type="bibr" rid="CIT0023">23</xref>) carried out research work on nuclear containment structure and found following empirical formula for peak pressure [<xref ref-type="disp-formula" rid="FD4">4</xref>]:<disp-formula id="FD4">
							<alternatives>
								<mml:math id="M4">
									<mml:mrow>
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											<mml:mi>p</mml:mi>
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												<mml:mi>o</mml:mi>
											</mml:mrow>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mn>1.017</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
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																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
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															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>1.91</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo>,</mml:mo>
										<mml:mn>12</mml:mn>
										<mml:mo>&#x2265;</mml:mo>
										<mml:msup>
											<mml:mrow>
												<mml:mo stretchy='false'>(</mml:mo>
												<mml:mtext>R</mml:mtext>
												<mml:mo>/</mml:mo>
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												<mml:mo stretchy='false'>)</mml:mo>
											</mml:mrow>
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												<mml:mn>1</mml:mn>
												<mml:mo>/</mml:mo>
												<mml:mn>3</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo>&#x2265;</mml:mo>
										<mml:mn>1</mml:mn>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>MPa</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq004.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<p>Experimental results by Ahmad et al. (<xref ref-type="bibr" rid="CIT0024">24</xref>) have generated the following relationship of P<sub>so</sub> with respect to the scaled distance [<xref ref-type="disp-formula" rid="FD5">5</xref>]:<disp-formula id="FD5">
							<alternatives>
								<mml:math id="M5">
									<mml:mrow>
										<mml:msub>
											<mml:mi>p</mml:mi>
											<mml:mrow>
												<mml:mi>s</mml:mi>
												<mml:mi>o</mml:mi>
											</mml:mrow>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mn>2.46</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>2.67</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>MPa</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq005.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<p>Whereas current research on brick masonry wall have suggested empirical attenuation relation for peak air pressure for a hemispherical shock wave front as under [<xref ref-type="disp-formula" rid="FD6">6</xref>]:<disp-formula id="FD6">
							<alternatives>
								<mml:math id="M6">
									<mml:mrow>
										<mml:msub>
											<mml:mi>p</mml:mi>
											<mml:mrow>
												<mml:mi>s</mml:mi>
												<mml:mi>o</mml:mi>
											</mml:mrow>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mn>3.495</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>3.408</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>MPa</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq006.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<p>Where R is standoff distance in meters measured from charge center and Q is TNT equivalent charge weight in kilograms. At different scaled distance peak air pressure determined by empirical formulae are given in <xref ref-type="table" rid="T0005">Table 5</xref>.
</p>
					<table-wrap id="T0005">
						<label>Table 5</label>
						<caption>
							<p>Comparison of Empirical Equations for P<sub>so</sub>
							</p>
						</caption>
						<table frame="hsides" rules="groups">
							<thead>
								<tr>
									<th align="left">Scaled Range (m/kg<sup>1/3</sup>)</th>
									<th align="center">Current Research</th>
									<th align="center">Saeed et al. (2012)</th>
									<th align="center">Siddiqui &#x0026; Ahmad (2007)</th>
									<th align="center">Wu and Hao (2005)</th>
									<th align="center">Brode (1955)</th>
									<th align="center">Hynrych and Major (1979)</th>
								</tr>
							</thead>
							<tbody>
								<tr>
									<td align="left">1.72</td>
									<td align="center">0.533</td>
									<td align="center">0.578</td>
									<td align="center">0.361</td>
									<td align="center">0.338</td>
									<td align="center">0.219</td>
									<td align="center">0.3906</td>
								</tr>
								<tr>
									<td align="left">1.81</td>
									<td align="center">0.4466</td>
									<td align="center">0.505</td>
									<td align="center">0.327</td>
									<td align="center">0.3058</td>
									<td align="center">0.1956</td>
									<td align="center">0.3678</td>
								</tr>
								<tr>
									<td align="left">2.07</td>
									<td align="center">0.28</td>
									<td align="center">0.353</td>
									<td align="center">0.253</td>
									<td align="center">0.234</td>
									<td align="center">0.1456</td>
									<td align="center">0.3153</td>
								</tr>
								<tr>
									<td align="left">2.2</td>
									<td align="center">0.227</td>
									<td align="center">0.2997</td>
									<td align="center">0.226</td>
									<td align="center">0.2066</td>
									<td align="center">0.1278</td>
									<td align="center">0.2945</td>
								</tr>
								<tr>
									<td align="left">2.24</td>
									<td align="center">0.2132</td>
									<td align="center">0.286</td>
									<td align="center">0.218</td>
									<td align="center">0.1993</td>
									<td align="center">0.1231</td>
									<td align="center">0.2887</td>
								</tr>
								<tr>
									<td align="left">2.28</td>
									<td align="center">0.201</td>
									<td align="center">0.272</td>
									<td align="center">0.211</td>
									<td align="center">0.1923</td>
									<td align="center">0.1186</td>
									<td align="center">0.283</td>
								</tr>
							</tbody>
						</table>
					</table-wrap>
					<p>Peak air pressures determined by present functions, by other empirical relations are then plotted in curves, expressed in <xref ref-type="fig" rid="F0013">Figure 13</xref>. As shown in <xref ref-type="fig" rid="F0013">Figure 13</xref>, for all scaled distances exponential decay of peak pressure of present research on brick wall are in close agreement with Siddiqui and Ahmad and Wu and Hao&#x2019;s results. Large variations of peak pressure are noticed with Henrych&#x2019;s curve. Brode (<xref ref-type="bibr" rid="CIT0013">13</xref>)&#x2019;s and Ahmad et al.&#x2019;s derived relations show similar behavior but peak pressures are quite different.</p>
					<fig id="F0013">
						<label>Figure 13</label>
						<caption>
							<p>Graph showing comparison of empirical equations for P<sub>so</sub>.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g013.tif"/>
					</fig>
				</sec>
				<sec>
					<title>3.4.4. Arrival time air blast wave</title>
					<p>The shock wave front arrival time T<sub>a</sub> is usually not included in the most of the studies on impulsive loading, are estimated here. Arrival time at different scaled distances is shown in <xref ref-type="fig" rid="F0014">Figure 14</xref>. As shown in this figure, with increasing scaled distance air blast wave arrival time decreases. Also it can be stated that at the same scaled distance, the smaller the explosive weight is, longer will be the arrival time. Empirical formula derived using experimental result for shock wave arrival time is [<xref ref-type="disp-formula" rid="FD7">7</xref>]:<disp-formula id="FD7">
							<alternatives>
								<mml:math id="M7">
									<mml:mrow>
										<mml:msub>
											<mml:mi>T</mml:mi>
											<mml:mi>a</mml:mi>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mfrac>
											<mml:mrow>
												<mml:mn>8.534</mml:mn>
											</mml:mrow>
											<mml:mrow>
												<mml:msub>
													<mml:mi>C</mml:mi>
													<mml:mi>a</mml:mi>
												</mml:msub>
											</mml:mrow>
										</mml:mfrac>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo stretchy="true">(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo stretchy="true">)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>0.996</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy="false">(</mml:mo>
										<mml:mtext>s</mml:mtext>
										<mml:mo stretchy="false">)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq007.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<fig id="F0014">
						<label>Figure 14</label>
						<caption>
							<p>Arrival time of air blast wave against scaled distance.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g014.tif"/>
					</fig>
					<p>Where arrival time of air blast wave is in seconds, R is the standoff in meters, and Q is the TNT equivalent charge weight in kg. C<sub>a</sub> is the velocity of sound in air, taken as 340 m/s. As shown in <xref ref-type="fig" rid="F0014">Figure 14</xref>, with increasing scaled distance air blast wave arrival time decreases. Also it can be stated that at the same scaled distance, the smaller the explosive weight is, longer will be the arrival time.</p>
				</sec>
				<sec>
					<title>3.4.5. Rising time of shock wave</title>
					<p>Rising time is defined as the time when pressure rises rapidly from ambient to peak pressure. In the literature, rising time is mostly not included as this time is very short. Pressure time wave is typically assumed starting from peak value and then exponentially decays to ambient value. For more accurate analysis of structures against blasting, rising time is considered in this study. Pressure increases exponentially from zero to peak value having a rising time T<sub>r</sub> shown in <xref ref-type="fig" rid="F0015">Figure 15</xref>. Derived empirical relationship using experimental data for rising time of shock wave is [<xref ref-type="disp-formula" rid="FD8">8</xref>]:<disp-formula id="FD8">
							<alternatives>
								<mml:math id="M8">
									<mml:mrow>
										<mml:msub>
											<mml:mi>T</mml:mi>
											<mml:mi>r</mml:mi>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mn>0.0014</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>0.759</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>s</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq008.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<fig id="F0015">
						<label>Figure 15</label>
						<caption>
							<p>Rising time of air blast wave against scaled distance.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g015.tif"/>
					</fig>
					<p>Where rising time is in seconds, R is the range in meters, and Q is the TNT equivalent charge weight in kg.</p>
				</sec>
				<sec>
					<title>3.4.6. Decreasing time of air blast wave</title>
					<p>Decreasing time is the time when pressure drops from peak to ambient value, another parameter for modeling of pressure time history shown in <xref ref-type="fig" rid="F0016">Figure 16</xref>. Based on experimental data the best-fitted relation is [<xref ref-type="disp-formula" rid="FD9">9</xref>]:<disp-formula id="FD9">
							<alternatives>
								<mml:math id="M9">
									<mml:mrow>
										<mml:msub>
											<mml:mi>T</mml:mi>
											<mml:mi>d</mml:mi>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mn>0.0005</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>2.159</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>s</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq009.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<fig id="F0016">
						<label>Figure 16</label>
						<caption>
							<p>Decreasing time of air blast wave against scaled distance.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g016.tif"/>
					</fig>
				</sec>
				<sec>
					<title>3.4.7. Positive phase duration of shock wave</title>
					<p>Positive phase duration is the summation of rising time and decreasing time.</p>
					<p>So it can be written as [<xref ref-type="disp-formula" rid="FD10">10</xref>]:<disp-formula id="FD10">
							<alternatives>
								<mml:math id="M10">
									<mml:mrow>
										<mml:msub>
											<mml:mi>T</mml:mi>
											<mml:mo>+</mml:mo>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:msub>
											<mml:mi>T</mml:mi>
											<mml:mi>r</mml:mi>
										</mml:msub>
										<mml:mo>+</mml:mo>
										<mml:msub>
											<mml:mi>T</mml:mi>
											<mml:mi>d</mml:mi>
										</mml:msub>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq010.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<p>Combining equation the positive phase duration is [<xref ref-type="disp-formula" rid="FD11">11</xref>]:<disp-formula id="FD11">
							<alternatives>
								<mml:math id="M11">
									<mml:mrow>
										<mml:mi>T</mml:mi>
										<mml:mo>=</mml:mo>
										<mml:mn>0.0014</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>0.759</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo>+</mml:mo>
										<mml:mn>0.0005</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mn>2.159</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>s</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq011.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<p>
						<xref ref-type="fig" rid="F0017">Figure 17</xref> is the graphical variation of positive phase duration against scaled distance.</p>
					<fig id="F0017">
						<label>Figure 17</label>
						<caption>
							<p>Positive phase duration against scaled distance.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g017.tif"/>
					</fig>
				</sec>
				<sec>
					<title>3.4.8. Peak reflected pressure</title>
					<p>In air blast pressure time history, when incident wave impinges with the structure e.g. wall it will reflect. When the blast wave is reflected against the perpendicular surface, it may result in enhanced intensity reflected pressure as compared to incident pressure wave. Design manual, UFC (<xref ref-type="bibr" rid="CIT0018">18</xref>) and AASTP (<xref ref-type="bibr" rid="CIT0019">19</xref>) chart provide curves to calculate peak reflected pressure from the peak incident air pressure. Various relationships of reflected pressure are also available in literature relating peak reflected pressure to the peak free incident air pressure. <xref ref-type="fig" rid="F0018">Figure 18</xref> shows comparison of UFC (<xref ref-type="bibr" rid="CIT0018">18</xref>), AASTP (<xref ref-type="bibr" rid="CIT0019">19</xref>) design manual with the empirical relationships of other researchers of peak reflected pressure and peak air pressure. As shown, that ratio increases with the increase in peak air pressure. Variation of design chart values with Siddiqui and Ahmad (<xref ref-type="bibr" rid="CIT0023">23</xref>) is due to the curved concrete structure. Henrych and Major (<xref ref-type="bibr" rid="CIT0014">14</xref>) and Wu and Hao (<xref ref-type="bibr" rid="CIT0022">22</xref>) show small variation this may be attributed to the numerical simulation results of pressure.</p>
					<fig id="F0018">
						<label>Figure 18</label>
						<caption>
							<p>Ratio of horizontal peak reflected pressure to the peak air pressure against peak air pressure.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g018.tif"/>
					</fig>
				</sec>
			</sec>
			<sec id="S20018">
				<title>3.5. Ground shock wave parameters</title>
				<p>Ground shock wave history is defined by its peak value, time of arrival of ground shock waves; duration and time difference in arrival of air blast and ground shock waves given in <xref ref-type="table" rid="T0006">Table 6</xref>. The Conwep software (<xref ref-type="bibr" rid="CIT0017">17</xref>) has been used for comparison of various ground shock parameters with the experimental values. This program calculates the peak free-field stress owing to the directly transmitted shock wave, and optionally allows the addition of a reflected wave from a deeper layer and a relief (tension) wave reflected from the ground surface. It is important to note that relief wave effects for high magnitude shocks and/or near surface detonations are not well understood, and inclusion of a relief wave in these situations may lead to un-conservative answers. Peak particle velocity, acceleration and displacement are calculated using the direct path only. Reflections from the surface or a lower layer are not included.
</p>
				<table-wrap id="T0006">
					<label>Table 6</label>
					<caption>
						<p>Experimental values of ground shock wave parameters</p>
					</caption>
					<table frame="hsides" rules="groups">
						<thead>
							<tr>
								<th align="left"/>
								<th align="center" colspan="6">GROUND SHOCK WAVE PARAMETERS</th>
							</tr>
							<tr>
								<th align="left"/>
								<th align="center" colspan="6"><hr/></th>
							</tr>
							<tr>
								<th align="left" rowspan="3" valign="bottom">Scaled distance (m/kg<sup>1/3</sup>)</th>
								<th align="center" colspan="2">PPA (m/s<sup>2</sup>)</th>
								<th align="center" colspan="2">t<sub>a</sub>(sec)</th>
								<th align="center" colspan="2">t<sub>d</sub>(sec)</th>
							</tr>
							<tr>
								<th align="center" colspan="2"><hr/></th>
								<th align="center" colspan="2"><hr/></th>
								<th align="center" colspan="2"><hr/></th>
							</tr>
							<tr>
								<th align="center">Experimental</th>
								<th align="center">ConWep</th>
								<th align="center">Experimental</th>
								<th align="center">ConWep</th>
								<th align="center">Experimental</th>
								<th align="center">ConWep</th>
							</tr>
						</thead>
						<tbody>
							<tr>
								<td align="left">1.72</td>
								<td align="center">186.865</td>
								<td align="center">109.1</td>
								<td align="center">0.0121</td>
								<td align="center">0.01303</td>
								<td align="center">0.05721</td>
								<td align="center">0.04962</td>
							</tr>
							<tr>
								<td align="left">1.81</td>
								<td align="center">112.678</td>
								<td align="center">94.72</td>
								<td align="center">0.01725</td>
								<td align="center">0.01293</td>
								<td align="center">0.046112</td>
								<td align="center">0.04478</td>
							</tr>
							<tr>
								<td align="left">2.07</td>
								<td align="center">151.742</td>
								<td align="center">65.32</td>
								<td align="center">0.012</td>
								<td align="center">0.01206</td>
								<td align="center">0.04378</td>
								<td align="center">0.04211</td>
							</tr>
							<tr>
								<td align="left">2.20</td>
								<td align="center">76.945</td>
								<td align="center">50.23</td>
								<td align="center">0.0119</td>
								<td align="center">0.01352</td>
								<td align="center">0.03911</td>
								<td align="center">0.04191</td>
							</tr>
							<tr>
								<td align="left">2.24</td>
								<td align="center">125.404</td>
								<td align="center">58.65</td>
								<td align="center">0.0105</td>
								<td align="center">0.01037</td>
								<td align="center">0.03639</td>
								<td align="center">0.037</td>
							</tr>
							<tr>
								<td align="left">2.28</td>
								<td align="center">90.81</td>
								<td align="center">50.18</td>
								<td align="center">0.00875</td>
								<td align="center">0.01193</td>
								<td align="center">0.03182</td>
								<td align="center">0.03007</td>
							</tr>
						</tbody>
					</table>
				</table-wrap>
				<sec>
					<title>3.5.1. Peak particle acceleration</title>
					<p>Peak particle acceleration is the maximum acceleration of acceleration time history graph. Experimental and ConWep obtained PPA for different charge weights are shown in <xref ref-type="fig" rid="F0019">Figure 19</xref>. Empirical relation of PPA provides the surface ground motion as a function of scaled distance is [<xref ref-type="disp-formula" rid="FD12">12</xref>]:<disp-formula id="FD12">
							<alternatives>
								<mml:math id="M12">
									<mml:mrow>
										<mml:mi>P</mml:mi>
										<mml:mi>P</mml:mi>
										<mml:mi>A</mml:mi>
										<mml:mo>=</mml:mo>
										<mml:mn>421.18</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo stretchy="true">(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo stretchy="true">)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>1.774</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy="false">(</mml:mo>
										<mml:mtext>m</mml:mtext>
										<mml:mo>/</mml:mo>
										<mml:msup>
											<mml:mtext>s</mml:mtext>
											<mml:mtext>2</mml:mtext>
										</mml:msup>
										<mml:mo stretchy="false">)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq012.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<fig id="F0019">
						<label>Figure 19</label>
						<caption>
							<p>Comparison of peak particle acceleration.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g019.tif"/>
					</fig>
				</sec>
				<sec>
					<title>3.5.2. Ground shock wave arrival time</title>
					<p>In modeling of simultaneous air blast and ground shock forces on structures, arrival time of ground shock motions is needed. Experimental values when plotted in <xref ref-type="fig" rid="F0020">Figure 20</xref> gave the following empirical equations [<xref ref-type="disp-formula" rid="FD13">13</xref>]:<disp-formula id="FD13">
							<alternatives>
								<mml:math id="M13">
									<mml:mrow>
										<mml:msub>
											<mml:mi>t</mml:mi>
											<mml:mi>a</mml:mi>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mfrac>
											<mml:mrow>
												<mml:mn>46.17</mml:mn>
											</mml:mrow>
											<mml:mrow>
												<mml:msub>
													<mml:mi>C</mml:mi>
													<mml:mi>s</mml:mi>
												</mml:msub>
											</mml:mrow>
										</mml:mfrac>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>1.32</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>s</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq013.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<fig id="F0020">
						<label>Figure 20</label>
						<caption>
							<p>Arrival time of ground shock wave.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g020.tif"/>
					</fig>
					<p>The soil possessed the following properties: Density = 1920 kg/m<sup>3</sup>, seismic velocity of the soil C<sub>s</sub>=1524 m/sec.</p>
				</sec>
				<sec>
					<title>3.5.3. Duration of ground shock wave</title>
					<p>An important parameter that appreciably affects the structural response against impulsive loading is the duration of shock wave in <xref ref-type="fig" rid="F0021">Figure 21</xref>. Shock wave duration is the difference of total ground shock wave time and time of arrival of ground motions [<xref ref-type="disp-formula" rid="FD14">14</xref>]:<disp-formula id="FD14">
							<alternatives>
								<mml:math id="M14">
									<mml:mrow>
										<mml:msub>
											<mml:mi>t</mml:mi>
											<mml:mi>a</mml:mi>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mi>T</mml:mi>
										<mml:mo>-</mml:mo>
										<mml:msub>
											<mml:mi>t</mml:mi>
											<mml:mi>a</mml:mi>
										</mml:msub>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq014.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<fig id="F0021">
						<label>Figure 21</label>
						<caption>
							<p>Ground shock wave duration.</p>
						</caption>
						<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g021.tif"/>
					</fig>
					<p>Empirical formula for shock wave duration [<xref ref-type="disp-formula" rid="FD15">15</xref>]:<disp-formula id="FD15">
							<alternatives>
								<mml:math id="M15">
									<mml:mrow>
										<mml:msub>
											<mml:mi>t</mml:mi>
											<mml:mi>a</mml:mi>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mn>0.1308</mml:mn>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>1.603</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>s</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq015.tif"/>
							</alternatives>
						</disp-formula>
					</p>
				</sec>
				<sec>
					<title>3.5.4. Time lag between air blast and ground shock wave</title>
					<p>Time lag is the difference between arrival time of air blast and ground shock wave.</p>
					<p>
						<italic>T</italic>
						<sub>
							<italic>lag</italic>
						</sub>
						<italic>=T</italic>
						<sub>
							<italic>a</italic>
						</sub>
						<italic>-t</italic>
						<sub>
							<italic>a</italic>
						</sub>
					</p>
					<p>Empirical relationship for T<sub>lag</sub> [<xref ref-type="disp-formula" rid="FD16">16</xref>]:<disp-formula id="FD16">
							<alternatives>
								<mml:math id="M16">
									<mml:mrow>
										<mml:msub>
											<mml:mi>T</mml:mi>
											<mml:mrow>
												<mml:mi>l</mml:mi>
												<mml:mi>a</mml:mi>
												<mml:mi>g</mml:mi>
											</mml:mrow>
										</mml:msub>
										<mml:mo>=</mml:mo>
										<mml:mfrac>
											<mml:mrow>
												<mml:mn>8.534</mml:mn>
											</mml:mrow>
											<mml:mrow>
												<mml:msub>
													<mml:mi>C</mml:mi>
													<mml:mi>a</mml:mi>
												</mml:msub>
											</mml:mrow>
										</mml:mfrac>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>0.996</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo>-</mml:mo>
										<mml:mfrac>
											<mml:mrow>
												<mml:mn>46.17</mml:mn>
											</mml:mrow>
											<mml:mrow>
												<mml:msub>
													<mml:mi>C</mml:mi>
													<mml:mi>s</mml:mi>
												</mml:msub>
											</mml:mrow>
										</mml:mfrac>
										<mml:msup>
											<mml:mrow>
												<mml:mrow>
													<mml:mo>(</mml:mo>
													<mml:mrow>
														<mml:mfrac>
															<mml:mi>R</mml:mi>
															<mml:mrow>
																<mml:msup>
																	<mml:mi>Q</mml:mi>
																	<mml:mrow>
																		<mml:mrow>
																			<mml:mn>1</mml:mn>
																			<mml:mo>/</mml:mo>
																			<mml:mn>3</mml:mn>
																		</mml:mrow>
																	</mml:mrow>
																</mml:msup>
															</mml:mrow>
														</mml:mfrac>
													</mml:mrow>
													<mml:mo>)</mml:mo>
												</mml:mrow>
											</mml:mrow>
											<mml:mrow>
												<mml:mo>-</mml:mo>
												<mml:mn>1.32</mml:mn>
											</mml:mrow>
										</mml:msup>
										<mml:mo stretchy='false'>(</mml:mo>
										<mml:mtext>s</mml:mtext>
										<mml:mo stretchy='false'>)</mml:mo>
									</mml:mrow>
								</mml:math>
								<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-eq016.tif"/>
							</alternatives>
						</disp-formula>
					</p>
					<p>The time lag between the ground shock and the blast wave shows that the air blast wave reaches the structure before the arrival of ground shocks for small-scaled distances. It was noticed that the time lag is not only related to scaled distance but also to wave propagation velocity in the air and at the site. The values of backfill density, seismic velocity and attenuation coefficient have been assumed on the basis of apparent characteristics of soil, which vary with distance and depth. Therefore, it should not be a matter of great concern if the experimental and ConWep results do not match closely.</p>
				</sec>
			</sec>
			<sec id="S20023">
				<title>3.6. Principal stresses</title>
				<p>Maximum and minimum principal stress plots of 45&#x00B0; strain rosette for selected element are shown in <xref ref-type="fig" rid="F0022">Figure 22</xref>. This figure illustrates stress plots of element, which was directly exposed, to the blast pressure. Principal stress &#x3C3;<sub>1</sub> for maximum (most tensile) or &#x3C3;<sub>2</sub> is for minimum (most compressive). As it can be seen that wall is subjected to either tension or compression failure. Wall has completely lost their lost carrying capacity as the principal stresses decreases after blast. Plots of principal stress can be used to find out the damage mechanism and the damage extent for estimation of residual capacity of structures subjected to blast.</p>
				<fig id="F0022">
					<label>Figure 22</label>
					<caption>
						<p>Plot of principal stress under explosive loads.</p>
					</caption>
					<graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="MC201310-e007-01513-g022.tif"/>
				</fig>
			</sec>
		</sec>
		<sec id="S0024">
			<title>4. CONCLUSIONS</title>
			<p>The following conclusions are drawn from this study:</p>
			<list list-type="bullet">
				<list-item><p>Peak pressure determined by experimental record agrees well with that from Con Wep, design manual, UFC and AASTP chart for hemispherical surface explosion. However, experimental results are comparatively more consistent with those as predicted by AASTP.</p>
					
				</list-item>
				<list-item>
			<p>For all scaled distances exponential decay of peak pressure show similar behaviour with previous researchers but quite different at small distance. This is due to difficulty in measuring overpressure at small scaled distances.</p>		
				</list-item>
				<list-item>
			<p>With increasing scaled distance air blast wave arrival time decreases. Also it can be stated that at the same scaled distance, the smaller the explosive weight is, longer will be the arrival time.</p>		
				</list-item>
				<list-item>
			<p>It was noted that the time lag is not only related to scaled distance but also to wave propagation velocity in the air and at the site.</p>		
				</list-item>
				<list-item><p>Consideration of both air blast and ground shock parameters can develop deep understanding of response of structure against explosion.</p>
				</list-item>
				<list-item><p>For a deeper understanding of response of masonry wall, there is a need for carrying out an extensive experimental work with charge weights of a number of intensities at various standoff distances.</p>
				</list-item>
			</list>
		</sec>
	</body>
	<back>
		<ref-list>
			<title>REFERENCES</title>
			<ref id="CIT0001">
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