Evaluation of test/analysis correlation methods for crash applications

Journal of the American Helicopter Society

Volumn 47, Issue 4, 2002, Pages 233-242

  Lyle, Karen H ^a   Bark, Lindley W ^a   Jackson, Karen E ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CORRELATION METHODS; FINITE ELEMENT METHOD; FUSELAGES;

CRASH TESTS;

FLIGHT DYNAMICS;

EID: 0036802919     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.47.233     Document Type: Article

References (8)

1. Bark, L.W., and Lyle, K.H., "Progress toward Understanding Correlation of Crash Test with Crash Simulation," Proceedings of the Third International KRASH Users' Seminar, Tempe, AZ, January 8-10, 2001.
2. Lyle, K.H., Bark, L.W., and Jackson, K.E., "Evaluation of Test/Analysis Correlation Methods for Crash Applications," American Helicopter Society 57th Annual Forum Proceedings, Washington, DC, May 9-11, 2001.
3. Vaughan, V.L., Jr., and Alfaro-Bou, E., "Impact Dynamics Research Facility for Full-Scale Aircraft Crash Testing," NASA TN D-8179, April 1976.
4. Society of Automotive Engineers, Recommended Practice: Instrumentation for Impact Test-Part 1, Electronic Instrumentation, SAE J211/1, March 1995.
5. Fasanella, E.L., Jackson, K.E., and Lyle, K.H., "Finite Element Simulation of a Full-Scale Crash Test of a Composite Helicopter," The American Helicopter Society 56th Annual Forum Proceedings, Virginia Beach, VA, May 2-4, 2000.
6. Jackson, K.E., and Fasanella, E.L., "Development of a Crashworthy Composite Fuselage Concept," Proceedings of the 2000 Advances in Aviation Safety Conference (P-355), Daytona Beach, FL, April 11-13, 2000.
7. Jackson, K.E., Fasanella, E.L., and Kellas, S., "Development of a Scale Model Composite Fuselage Concept for Improved Crashworthiness," Journal of Aircraft, Vol. 38, (1), January-February 2000, pp. 95-103.
8. Stech, E.L., and Payne, P.R., "Dynamic Models of the Human Body," Frost Engineering and Development Corporation, AMRL Technical Report 66-158, Aerospace Medical Research Laboratory, Wright-Patterson AFB, OH, November 1969.