Control of unsteady separated flow associated with the dynamic stall of airfoils
Subtitle: final report, 95-09
By: M.C. Wilder.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-198972.
Publisher: MCAT Institute; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: San Jose, CA; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic stalling.; Airfoil oscillations.; Airfoil profiles.; Boundary layer control.; Boundary layer separation.; Leading edges.; Mach number.; Reynolds number.; Supercritical airfoils.; Unsteady flow.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0038-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.