scholarly journals A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft

2015 ◽  
Vol 2015 ◽  
pp. 1-8 ◽  
Author(s):  
Sebastian Heimbs ◽  
Josef Ritzer ◽  
Johannes Markmiller

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) ◽  
pp. 442-449 ◽  
Author(s):  
Kamran Khalifehei

Underwater explosion is a subject that has been paid attention to by many researchers. In this study the underwater explosion phenomena under shockwave loading is explored by numerical method. For this purpose, by modeling a marine pipe buried in the water by ABAQUS software, the effect of the shock wave and the damages were assessed. Then using the laboratorial results, the fluid-structure interaction and shock wave loading and its results were analysed. Finally, it was concluded from numerical modeling that the highest levels of strain on the pipe buried in the water under underwater explosion and shock wave loading occur in the ending parts of the pipe in both sides and away from explosion field.


2002 ◽  
Vol 82 (12) ◽  
pp. 2419-2440
Author(s):  
S. Golyandin ◽  
S. Kustov ◽  
S. Nikanorov ◽  
K. Sapozhnikov ◽  
A. Sinani ◽  
...  

2016 ◽  
Vol 117 (9) ◽  
pp. 962-968 ◽  
Author(s):  
N. N. Popov ◽  
V. F. Lar’kin ◽  
V. A. Ogorodnikov ◽  
D. V. Presnyakov ◽  
Yu. A. Lar’kina ◽  
...  

Author(s):  
Larysa Sudnik ◽  
Aleksey Luchenok ◽  
Yuliya Kaladkevich ◽  
Victor Tkachuk ◽  
Tatiana Prikhna ◽  
...  

1987 ◽  
Vol 5 (3) ◽  
pp. 75-78 ◽  
Author(s):  
I.K. Simonsen ◽  
Y. Horie ◽  
R.A. Graham ◽  
M. Carr

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