Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction
By: A.V. Murthy ... [et al.]
Contributors: Murthy, A. V; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical paper -- 2096
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: 47
Subjects: Boundary layer control; Wind tunnels -- Flow visualization
Notes: "Langley Research Center."

"March 1983"--Cover

Subject category 34

Includes bibliographical references