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Unitized composite fuselage fuel tank
29th Structures, Structural Dynamics and Materials Conference, 1988A unitized fuselage fuel tank has been designed, developed and fabricated using carbon/bismaleimide material. This tank reduces weight, detail parts, fasteners and assembly costs as compared to both metal construction and conventional composite construction. Multiple sub-element tests were run and a new tooling concept was developed prior to full scale
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MOVING TO COMPOSITE FUSELAGE DESIGN
2013This paper outlines the conception of the composite stiffened panel designed to shear and bending loading under post buckling behaviour.
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Fuselage-wing interference drag of aircraft with relatively short, pod-type, fuselages
40th AIAA Aerospace Sciences Meeting & Exhibit, 2002J. Kentfield, H. Jones
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