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Occupant Responses in a Full-Scale Crash Test of the Sikorsky ACAP HelicopterA full-scale crash test of the Sikorsky Advanced Composite Airframe Program (ACAP) helicopter was performed in 1999 to generate experimental data for correlation with a crash simulation developed using an explicit nonlinear, transient dynamic finite element code. The airframe was the residual flight test hardware from the ACAP program. For the test, the aircraft was outfitted with two crew and two troop seats, and four anthropomorphic test dummies. While the results of the impact test and crash simulation have been documented fairly extensively in the literature, the focus of this paper is to present the detailed occupant response data obtained from the crash test and to correlate the results with injury prediction models. These injury models include the Dynamic Response Index (DRI), the Head Injury Criteria (HIC), the spinal load requirement defined in FAR Part 27.562(c), and a comparison of the duration and magnitude of the occupant vertical acceleration responses with the Eiband whole-body acceleration tolerance curve.
Document ID
20030000682
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Jackson, Karen E.
(NASA Langley Research Center Hampton, VA United States)
Fasanella, Edwin L.
(NASA Langley Research Center Hampton, VA United States)
Boitnott, Richard
(NASA Langley Research Center Hampton, VA United States)
McEntire, Joseph
(Army Aeromedical Research Lab. Fort Rucker, AL United States)
Lewis, Alan
(Army Aeromedical Research Lab. Fort Rucker, AL United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Air Transportation And Safety
Meeting Information
Meeting: American Helicopter Society 58th Annaul Forum
Location: Montreal
Country: Canada
Start Date: June 11, 2002
End Date: June 13, 2002
Sponsors: American Helicopter Society, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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