Minimum weight design of a generic axisymmetric inlet
By: Shari-Beth Nadell.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 107288.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Symmetry.; Air intakes.; Finite element method.; Supersonic inlets.; Structural design.; Structural weight.; Engine design.
Notes: Shipping list no.: 98-0783-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.