Report presents overview of research involving use of concepts of aircraft elements and substructures not necessarily designed or optimized with respect to energy-absorption or crash-loading considerations. Experimental and analytical data presented in report indicate some general trends in failure behaviors of class of composite-material structures including individual fuselage frames, skeleton subfloors with stringers and floor beams but without skin covering, and subfloors with skin added to frame/stringer arrangement.
Behavior Of Aircraft Components Under Crash-Type Loads
NASA Tech Briefs ; 17 , 8
1993-08-01
Miscellaneous
No indication
English
Failure Of Aircraft Components Under Crash-Type Loads
NTRS | 1993
|NTIS | 1967
|TIBKAT | 2001