Methods of achieving crash-worthiness of aircraft in general are discussed. Specific conclusions are drawn with regard to the design loads for occupant restraint systems. A “ programmed break” concept for the fuselage of large aircraft is presented, and additional research which is needed to provide increased survival in accidents is suggested.
Safety Engineering for Crash Injury Prevention
Sae Technical Papers
SAE World Congress & Exhibition ; 1964
1964-01-01
Conference paper
English
Safety engineering for crash injury prevention
Engineering Index Backfile | 1964
|Greater safety through crash injury analyses
Engineering Index Backfile | 1957
|Options for prevention of motor vehicle crash injury
Tema Archive | 1980
|