Evaluation of turbulance reduction devices for the Langley 8-Foot Transonic Pressure Tunnel
By: Marion O. McKinney and James Scheiman
Contributors: Scheiman, James; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical memorandum -- 81792
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 30
Subjects: Transonic wind tunnels; Laminar flow
Notes: "Langley Research Center."

"June 1981"--Cover

Subject category 09

Includes bibliographical references