Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
By: William D. Deveikis
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2127
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 92
Subjects: Aerothermodynamics; Heat -- Transmission; Aerodynamic load
Notes: Distributed to depository libraries in microfiche

"June 1983"--Cover

Includes bibliographical references