Development of Airframe Design Technology for Crashworthiness

730319

02/01/1973

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
This paper describes the NASA portion of a joint FAA-NASA General Aviation Crashworthiness Program leading to the development of improved crashworthiness design technology. The objectives of the program are to develop analytical technology for predicting crashworthiness of structures, provide design improvements, and perform full-scale crash tests. The analytical techniques which are being developed both in-house and under contract are described and typical results from these analytical programs are shown. In addition, the full-scale testing facility and test program are discussed.
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DOI
https://doi.org/10.4271/730319
Pages
4
Citation
Kruszewski, E., and Thomson, R., "Development of Airframe Design Technology for Crashworthiness," SAE Technical Paper 730319, 1973, https://doi.org/10.4271/730319.
Additional Details
Publisher
Published
Feb 1, 1973
Product Code
730319
Content Type
Technical Paper
Language
English