Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition
By: Robert W. Hess ... [et al.].
Contributors: Hess, R. W.; Langley Research Center.
Series: NASA technical memorandum -- 89080.
Publisher: National Aeronautics and Space Administration, Langley Research Center; For sale by the National Technical Information Service
Published: 1987
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Reynolds number.; Mach number.; Aerodynamics.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche.