Application study of filamentary composites in a commercial jet aircraft fuselage [PDF]
A study of applications of filamentary composite materials to aircraft fuselage structure was performed. General design criteria were established and material studies conducted using the 727-200 forebody as the primary structural component.
Johnson, R. W., June, R. R.
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Cost-Effectiveness of Structural Health Monitoring in Aviation: A Literature Review. [PDF]
Sensors (Basel)Ballarin P, Sala G, Airoldi A.
europepmc +1 more source
Skin, stringer, and fastener loads in buckled fuselage panels [PDF]
19th AIAA Applied Aerodynamics Conference, 2001 R. Young, C. Rose, K. Starnes, Jr.
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Geometrically nonlinear high-fidelity aerostructural optimization for highly flexible wings. [PDF]
Struct Multidiscipl OptimGray AC, Kennedy GJ, Martins JRRA.
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Test results for composite specimens and elements containing joints and cutouts [PDF]
A program was conducted to develop the technology for joints and cutouts in a composite fuselage that meets all design requirements of a large transport aircraft for the 1990s.
Hawley, A. V. +2 more
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Aerodynamic Effects of a Blended Multi-Winglet on an Airliner in Subsonic and Transonic Regimes. [PDF]
Biomimetics (Basel)Kobayashi E +3 more
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Wind tunnel tests of high-lift systems for advanced transports using high-aspect-ratio supercritical wings [PDF]
The wind tunnel testing of an advanced technology high lift system for a wide body and a narrow body transport incorporating high aspect ratio supercritical wings is described.
Allen, J. B. +2 more
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Emerging Materials for Durable and Sustainable Design of Aeronautic Structures. [PDF]
Materials (Basel)Carvalho P, Aguiar-Branco J, Guedes RM.
europepmc +1 more source
An overview of the crash dynamics failure behavior of metal and composite aircraft structures [PDF]
An overview of failure behavior results is presented from some of the crash dynamics research conducted with concepts of aircraft elements and substructure not necessarily designed or optimized for energy absorption or crash loading considerations ...
Boitnott, Richard L. +3 more
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Evaluation of smart SATCOM fuselage panel development
Report containing details of coupon, detail and full scale structural evaluation of the results for the composite panel, RF results evaluation including installed antenna performance and thermal evaluation results. Involved partners will provide detailed input in the form of a chapter containing the results to the leading contractor who will integrate
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