NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel /
Renaldo V. Jenkins.

Description

Main Author: Jenkins, Renaldo V.
Related Names: United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Subjects: Wind tunnels.
Reynolds number.
Boundary layer.
Aerofoils.
Note: "March 1989"--Cover.
Physical Description: 55 p. : ill. ; 28 cm.
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Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign