Body and canard effects on an attached-flow maneuver wing at Mach 1.62
By: James L. Pittman and David S. Miller, William H. Mason
Contributors: Miller, D. S.; Mason, William H. 1947-; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2249
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1984
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 145
Subjects: Airplanes -- Wings, Canard; Aerodynamics, Supersonic
Notes: Distributed to depository libraries in microfiche

"February 1984"--Cover

Includes bibliographical references