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NASA General Aviation Crashworthiness Seat Development

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Fasanella, Edwin L., author.
Conference Name:
Business Aircraft Meeting and Exposition (1979-04-03 : Wichita, Kansas, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1979
Summary:
Three load limiting seat concepts for general aviation aircraft designed to lower the deceleration of the occupant in the event of a crash were sled tested and evaluated with reference to a standard seat. Dummy pelvis accelerations were reduced up to 50 percent with one of the concepts.Computer program MSOMLA (Modified Seat Occupant Model for Light Aircraft) was used to simulate the behavior of a dummy passenger in a NASA full-scale crash test of a twin engine light aircraft. A computer graphics package MANPLOT was developed to pictorially represent the occupant and seat motion
Notes:
Vendor supplied data
Publisher Number:
790591
Access Restriction:
Restricted for use by site license

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