A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft
Joint Authors
Heimbs, Sebastian
Ritzer, Josef
Markmiller, Johannes
Source
International Journal of Aerospace Engineering
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-8, 8 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-09-30
Country of Publication
Egypt
No. of Pages
8
Abstract EN
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.
American Psychological Association (APA)
Heimbs, Sebastian& Ritzer, Josef& Markmiller, Johannes. 2015. A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft. International Journal of Aerospace Engineering،Vol. 2015, no. 2015, pp.1-8.
https://search.emarefa.net/detail/BIM-1064551
Modern Language Association (MLA)
Heimbs, Sebastian…[et al.]. A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft. International Journal of Aerospace Engineering No. 2015 (2015), pp.1-8.
https://search.emarefa.net/detail/BIM-1064551
American Medical Association (AMA)
Heimbs, Sebastian& Ritzer, Josef& Markmiller, Johannes. A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft. International Journal of Aerospace Engineering. 2015. Vol. 2015, no. 2015, pp.1-8.
https://search.emarefa.net/detail/BIM-1064551
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1064551
