Minimum weight design of a generic axisymmetric inlet / Shari-Beth Nadell.

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Bibliographic Details
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Main Author:	Nadell, Shari-Beth (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
Series:	NASA technical memorandum ; 107288.
Subjects:	Symmetry. Air intakes. Finite element method. Supersonic inlets. Structural design. Structural weight. Engine design.

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Call Number:	NAS 1.15:107288
NAS 1.15:107288	Available