Minimum weight design of a generic axisymmetric inlet /

Bibliographic Details
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.
Online Access:	https://purl.fdlp.gov/GPO/gpo67123

Description
Item Description:	Title from title screen (viewed April 20, 2016). "Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996." "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
Physical Description:	1 online resource (13 pages) : illustrations.
Bibliography:	Includes bibliographical references (page 9).