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Behavior Of Aircraft Components Under Crash-Type Loads
- Source :
- NASA Tech Briefs. 17(8)
- Publication Year :
- 1993
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1993.
-
Abstract
- 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.
- Subjects :
- Materials
Subjects
Details
- Language :
- English
- ISSN :
- 0145319X
- Volume :
- 17
- Issue :
- 8
- Database :
- NASA Technical Reports
- Journal :
- NASA Tech Briefs
- Publication Type :
- Report
- Accession number :
- edsnas.19930000485
- Document Type :
- Report