Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
By: Thomas A. Byrdsong and Cuyler W. Brooks, Jr
Contributors: Brooks, Cuyler W; Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 84614
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: 211
Subjects: Wind tunnels; Aerodynamic load; Airplanes -- Wings
Notes: "Langley Research Center."

Distributed to depository libraries in microfiche

"June 1983"--Cover

Includes bibliographical references