Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

Bibliographic Details
Corporate Authors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Other Authors: Murthy, A. V.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1983.
Series:NASA technical paper ; 2096.
Subjects:
Boundary layer control.
Wind tunnels > Flow visualization.

Evans: US Documents Microfiche (3rd floor)

Holdings details from Evans: US Documents Microfiche (3rd floor)
Call Number: NAS 1.60:2096
 
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NAS 1.60:2096 Available