TY  - JOUR
PY  - 2015//
TI  - A numerical method for blast shock wave analysis of missile launch from aircraft
JO  - International journal of aerospace engineering
A1  - Heimbs, Sebastian
A1  - Ritzer, Josef
A1  - Markmiller, Johannes
SP  - 1
EP  - 8
VL  - 2015
IS  - 
N2  - 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.<p />  <p>Language: en</p>
LA  - en
SN  - 1687-5966
UR  - http://dx.doi.org/10.1155/2015/897213
ID  - ref1
ER  -