1968
DOI: 10.1063/1.1692177
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Intermediate Strength Blast Wave

Abstract: Equations for the trajectory and overpressure of the shock front of the intermediate strength blast wave (10 < Δp/p0 ⪝ 0.02) are developed for spherical, cylindrical, and plane blasts. These equations are based on the correct limit method that provided the trajectory of the blast wave from the inverse pinch to velocities below Mach number 1.16 (Δp/p0 = 0.4). The correct limit equations are an extension of the strong shock similarity solution of G. I. Taylor for the spherical blast and A. Sakurai and S. … Show more

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Cited by 97 publications
(34 citation statements)
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“…Figure 6 taken from Obed Samuelraj et al 25 shows the comparison between the experimental NONEL blast wave trajectory with the ideal blast wave theory proposed by Jones. 24 The figure shows that the trajectory of the blast wave measured along the tube axis follows the trend well. Figure 7 shows the setup used to measure the total pressure behind the porous plates.…”
Section: Nonel Tubesmentioning
confidence: 68%
See 1 more Smart Citation
“…Figure 6 taken from Obed Samuelraj et al 25 shows the comparison between the experimental NONEL blast wave trajectory with the ideal blast wave theory proposed by Jones. 24 The figure shows that the trajectory of the blast wave measured along the tube axis follows the trend well. Figure 7 shows the setup used to measure the total pressure behind the porous plates.…”
Section: Nonel Tubesmentioning
confidence: 68%
“…24 This theory was proposed for blast waves of intermediate strength (10> Áp/p 0 5 0.02, where Áp is the overpressure). Figure 6 taken from Obed Samuelraj et al 25 shows the comparison between the experimental NONEL blast wave trajectory with the ideal blast wave theory proposed by Jones.…”
Section: Nonel Tubesmentioning
confidence: 98%
“…An estimate of the sensitivity of ground damage to energy deposition profiles can be obtained from the characteristic distance of an explosion. To have a similar blast footprint, the energy deposition profile needs to have similar energies deposited within a fraction of the characteristic distance, which is given by Jones [] as Rchar=()5225.34γPnormalatmE13, where γ and P atm are the ratio of specific heats and pressure of the surrounding air and E is the explosive energy released. For a static explosion equivalent to Chelyabinsk, with an energy of 500 kt of TNT at 30 km altitude, the characteristic distance is 35 km.…”
Section: Resultsmentioning
confidence: 99%
“…Thermal properties of aluminum are given in Table 1 [38,39,40]. The constant, A, in the equation for the density of liquid aluminum is 0.35 [41]. The specific heat ratios of aluminum vapor which is assumed to be a monatomic gas and the ambient gas, air, are taken to be [43].…”
Section: Resultsmentioning
confidence: 99%