A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft
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,...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
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Wiley
2015-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2015/897213 |
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| _version_ | 1849411562908942336 |
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| author | Sebastian Heimbs Josef Ritzer Johannes Markmiller |
| author_facet | Sebastian Heimbs Josef Ritzer Johannes Markmiller |
| author_sort | Sebastian Heimbs |
| collection | DOAJ |
| description | 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. |
| format | Article |
| id | doaj-art-5ddac7dd3bba461a94be8605cee530d6 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2015-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-5ddac7dd3bba461a94be8605cee530d62025-08-20T03:34:44ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742015-01-01201510.1155/2015/897213897213A Numerical Method for Blast Shock Wave Analysis of Missile Launch from AircraftSebastian Heimbs0Josef Ritzer1Johannes Markmiller2Department of Structure Engineering, Production and Aeromechanics, Airbus Group Innovations, Willy-Messerschmitt-Strasse, 85521 Ottobrunn, GermanyDepartment of Structure Engineering, Production and Aeromechanics, Airbus Group Innovations, Willy-Messerschmitt-Strasse, 85521 Ottobrunn, GermanyDepartment of Stress, Loads and Crash, Airbus Helicopters, Industriestrasse 4, 86609 Donauwörth, GermanyAn 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.http://dx.doi.org/10.1155/2015/897213 |
| spellingShingle | Sebastian Heimbs Josef Ritzer Johannes Markmiller A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft International Journal of Aerospace Engineering |
| title | A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft |
| title_full | A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft |
| title_fullStr | A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft |
| title_full_unstemmed | A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft |
| title_short | A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft |
| title_sort | numerical method for blast shock wave analysis of missile launch from aircraft |
| url | http://dx.doi.org/10.1155/2015/897213 |
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