Subsonic and supersonic longitudinal stability and control characteristics of an aft tail fighter configuration with cambered and uncambered wings and cambered fuselage / by Samuel M. Dollyhigh.

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Main Author: Dollyhigh, Samuel M.
Corporate Authors: Langley Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974.
Series:NASA technical memorandum ; X-3078.
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Norlin Library - Government Information - US

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Call Number: NAS 1.15:3078
NAS 1.15:3078 Available Place a Hold