Ninth DOD/NASA/FAA Conference on Fibrous Composites in Structural Design, volume 3This publication contains the proceedings of the Ninth DOD/NASA/FAA Conference on Fibrous Composites in Structural Design held at Lake Tahoe, Nevada, during 4-7 Nov. 1991. Presentations were made in the following areas of composite structural design: perspectives in composites, design methodology, design applications, design criteria, supporting technology, damage tolerance, and manufacturing.
Document ID
19950021845
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Soderquist, Joseph R. (Federal Aviation Administration Washington, DC, United States)
Neri, Lawrence M. (Federal Aviation Administration Atlantic City, NJ., United States)
Bohon, Herman L. (Galaxy Scientific Corp. Hampton, VA., United States)
IDRelationTitle19950022000WorkUtilization of composite materials by the US Army: A look ahead19950022001WorkBenefits and limitations of composites in carrier-based aircraft19950022002WorkMechanical properties of triaxially braided composites: Experimental and analytical results19950022003WorkMechanisms of compressive failure in woven composites and stitched laminates19950022004WorkEffect of the fiber-matrix interphase on the transverse tensile strength of the unidirectional composite material19950022005WorkThe effect of material heterogeneity in curved composite beams for use in aircraft structures19950022006WorkInvestigation of static and cyclic bearing failure mechanisms for GR/EP laminates19950022007WorkCompression failure of angle-ply laminates19950022008WorkAnalysis of composite structures with delaminations under combined bending and compression19950022009WorkBuckling behavior of long symmetrically laminated plates subjected to combined loads19950022010WorkCompressive residual strength of graphite/epoxy laminates after impact19950022011WorkApplication of advanced material systems to composite frame elements19950022012WorkDesign, analysis, and testing of a metal matrix composite web/flange intersection19950022013WorkCharacteristics of laminates with delamination control strips19950022014WorkVibrational behavior of adaptive aircraft wing structures modelled as composite thin-walled beams19950022015WorkUnique considerations in the design and experimental evaluation of tailored wings with elastically produced chordwise camber19950022016WorkC-130 Advanced Technology Center wing box conceptual design/cost study19950022017WorkDevelopment of composite carrythrough bulkhead19950022018WorkEffects of floor location on response of composite fuselage frames19950022019WorkStructural design optimization with survivability dependent constraints application: Primary wing box of a multi-role fighter19950022020WorkReliability analysis of composite structures19950022021WorkUncertainties in obtaining high reliability from stress-strength models19950022022WorkProbabilistic design of advanced composite structure19950022023WorkProbabilistic evaluation of fuselage-type composite structures19950022024WorkProof test methodology for composites19950022025WorkNavy composite maintenance and repair experience