Supersonic stability and control characteristics of a cruciform missile model with delta wings and aft tail fin controls
By: William A. Corlett
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical memorandum -- 80171
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; for sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 115
Subjects: Aerodynamics, Supersonic; Airplanes -- Wings, Cruciform; Stress-strain curves
Notes: "December 1979"-- Cover

"Langley Research Center."

Includes bibliographical reference