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Best Practices for Crash Modeling and SimulationAviation safety can be greatly enhanced by the expeditious use of computer simulations of crash impact. Unlike automotive impact testing, which is now routine, experimental crash tests of even small aircraft are expensive and complex due to the high cost of the aircraft and the myriad of crash impact conditions that must be considered. Ultimately, the goal is to utilize full-scale crash simulations of aircraft for design evaluation and certification. The objective of this publication is to describe "best practices" for modeling aircraft impact using explicit nonlinear dynamic finite element codes such as LS-DYNA, DYNA3D, and MSC.Dytran. Although "best practices" is somewhat relative, it is hoped that the authors' experience will help others to avoid some of the common pitfalls in modeling that are not documented in one single publication. In addition, a discussion of experimental data analysis, digital filtering, and test-analysis correlation is provided. Finally, some examples of aircraft crash simulations are described in several appendices following the main report.
Document ID
20020085101
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Fasanella, Edwin L.
(Army Research Lab. Hampton, VA United States)
Jackson, Karen E.
(Army Research Lab. Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2002
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARL-TR-2849
NAS 1.15:211944
NASA/TM-2002-211944
L-18223
Report Number: ARL-TR-2849
Report Number: NAS 1.15:211944
Report Number: NASA/TM-2002-211944
Report Number: L-18223
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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