Study of advanced composite structural design concepts for an arrow wing supersonic cruise configuration / M. J. Turner and D. L. Grande, Boeing Commercial Airplane Company.

Based on estimated graphite and boron fiber properties, allowable stresses and strains were established for advanced composite materials. Stiffened panel and conventional sandwich panel concepts were designed and analyzed, using graphite/polyimide and boron/polyimide materials. The conventional san...

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Main Author: Turner, M. J.
Corporate Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Boeing Commercial Airplane Company, Langley Research Center
Other Authors: Grande, D. L.
Format: Government Document Book
Language:English
Published: [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978.
Series:NASA contractor report ; NASA CR-2825.
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