A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft
| Autor: | Sebastian Heimbs, Josef Ritzer, Johannes Markmiller |
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| Jazyk: | angličtina |
| Rok vydání: | 2015 |
| Předmět: | |
| Zdroj: | International Journal of Aerospace Engineering, Vol 2015 (2015) |
| Druh dokumentu: | article |
| ISSN: | 1687-5966 1687-5974 |
| DOI: | 10.1155/2015/897213 |
| Popis: | 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. |
| Databáze: | Directory of Open Access Journals |
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