Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds
By: Robert L. Stallings, Jr., Milton Lamb, and Carolyn B. Watson
Contributors: Lamb, Milton; Watson, Carolyn B; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical paper -- 1683
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 108
Subjects: Airplanes -- Wings; Stability of airplanes
Notes: "July 1980"--Cover

"Langley Research Center."

Includes bibliographical references