Occupant Impact Injury Tolerances for Aircraft Crashworthiness Design

710406

02/01/1971

Event
International Mid-Year Meeting
Authors Abstract
Content
Human impact injury and survival tolerance levels for various crash conditions are presented on the basis of currently available biomedical and biomechanical knowledge. Consideration of physical factors influencing trauma-including body orientation, restraint system, magnitude, distribution, and time duration of deceleration-are summarized, as well as tabulations and sources of data for both whole body and regional impact tolerances. These biological data concerning human impact tolerances are provided as guidelines for improved engineering design of general aviation crashworthiness.
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DOI
https://doi.org/10.4271/710406
Pages
20
Citation
Snyder, R., "Occupant Impact Injury Tolerances for Aircraft Crashworthiness Design," SAE Technical Paper 710406, 1971, https://doi.org/10.4271/710406.
Additional Details
Publisher
Published
Feb 1, 1971
Product Code
710406
Content Type
Technical Paper
Language
English