2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
By: R.A. Piziali.
Contributors: Ames Research Center.; U.S. Army Aviation and Troop Command.
Series: NASA technical memorandum -- 4632; USAATCOM technical report -- 94-A-011
Publisher: National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command; National Technical Information Service, distributor
Published: 1994
Place of publication: Moffett Field, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic coefficients.; Aerodynamic stalling.; Airfoils.; Angle of attack.; Pressure distribution.; Rotary wings.; Semispan models.; Wind tunnel tests.; Wind oscillations.
Other titles: 2 D and 3 D oscillating wing aerodynamics for a range of angles of attack including stall
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0410-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 6 microfiches.