Effect of acoustic excitation on stalled flows over an airfoil
By: K.B.M.Q. Zama.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 103183.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1990
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Acoustic excitation.; Aerodynamic stalling.; Airfoil profiles.; Boundary layer separation.; Flow distribution.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.