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.
Development of airframe design technology for crashworthiness.
Business Aircraft Meeting ; 1973 ; Wichita, KS
1973-04-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Development of Airframe Design Technology for Crashworthiness
SAE Technical Papers | 1973
|Design and Test of an Improved Crashworthiness Small Composite Airframe
British Library Conference Proceedings | 2000
|Design and Test of an Improved Crashworthiness Small Composite Airframe
SAE Technical Papers | 2000
|