@article{ref1,
title="A numerical method for blast shock wave analysis of missile launch from aircraft",
journal="International journal of aerospace engineering",
year="2015",
author="Heimbs, Sebastian and Ritzer, Josef and Markmiller, Johannes",
volume="2015",
number="",
pages="1-8",
abstract="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>",
language="en",
issn="1687-5966",
doi="10.1155/2015/897213",
url="http://dx.doi.org/10.1155/2015/897213"
}