Force and moment flow-visualization, and boundary-layer tests on a Shuttle Orbiter model at Mach 6
By: Robert L. Calloway
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 1952
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va. : For sale by the National Technical Information Service]
Language: eng
Number of pages: 23
Subjects: Reusable space vehicles -- Testing; Boundary layer -- Testing; Wind tunnels -- Testing
Notes: "Langley Research Center."

"December 1981"--Cover

Subject Category 02

Includes bibliographical references