Effect of wing location and strakes on stability and control characteristics of a monoplanar circular missile with low-profile tail fins at supersonic speeds
By: A.B. Blair, Jr.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Langley Research Center.
Series: NASA technical memorandum -- 81878.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 197
Subjects: Guided missiles -- Wings.; Supersonic wind tunnels.; Rolling (Aerodynamics); Yawing (Aerodynamics); Stability of airplanes, Lateral.
Notes: "Langley Research Center."

Dec. 1980.

Includes bibliographical references.