Supersonic stability and control characteristics of a cruciform missile model with delta wings and aft tail fin controls / William A. Corlett.

Bibliographic Details
Uniform Title:	NASA technical memorandum ; 80171.
Main Author:	Corlett, William A.
Corporate Authors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch Langley Research Center
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [for sale by the National Technical Information Service], 1979.
Series:	NASA technical memorandum ; 80171.
Subjects:	Aerodynamics, Supersonic. Airplanes > Wings, Cruciform. Stress-strain curves.
Physical Description:	115 unnumbered pages : illustrations ; 27 cm.
Format:	Government Document Microfilm Book

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