Pressure distributions from high Reynolds number transonic tests of an NACA 0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
By: Charles L. Ladson, Acquilla S. Hill, and William G. Johnson, Jr.
Contributors: Hill, Acquilla S.; Johnson, William G. 1944-; Langley Research Center.
Series: NASA technical memorandum -- 100526.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1988
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Aerodynamics, Transonic.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 5 microfiches.