A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft
2015 ◽
Vol 2015
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pp. 1-8
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Keyword(s):
An efficient empirical approach was developed to accurately represent the blast shock wave loading resulting from the launch of a missile from a military aircraft to be used in numerical analyses. Based on experimental test series of missile launches in laboratory environment and from a helicopter, equations were derived to predict the time- and position-dependent overpressure. The method was finally applied and validated in a structural analysis of a helicopter tail boom under missile launch shock wave loading.
2017 ◽
Vol 3
(6)
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pp. 442-449
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Keyword(s):
2020 ◽
Vol 1709
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pp. 012004
2016 ◽
Vol 117
(9)
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pp. 962-968
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Keyword(s):
2017 ◽
Vol 175
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pp. 012030
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Keyword(s):