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Unitized composite fuselage fuel tank

29th Structures, Structural Dynamics and Materials Conference, 1988
A 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

2013
This paper outlines the conception of the composite stiffened panel designed to shear and bending loading under post buckling behaviour.
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Fuselages

2010
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Optimal fuselage aiming

7th Computational Fluid Dynamics Conference, 1985
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Fuselage Design

Valentin A. Kiselev   +1 more
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Fuselage-wing interference drag of aircraft with relatively short, pod-type, fuselages

40th AIAA Aerospace Sciences Meeting & Exhibit, 2002
J. Kentfield, H. Jones
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