Wind-tunnel survey of an oscillating flow field for application to model helicopter rotor testing
By: Paul A. Mirick, M-Nabil H. Hamouda, William T. Yeager.
Contributors: Hamouda, M-Nabil H.; Yeager, William T.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4224.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1990
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aeroelasticity.; Flow distribution.; Gust loads.; Helicopter performance.; Oscillating flow.; Wind tunnel tests.
Other titles: Wind tunnel survey of an oscillating flow field for applciation to model helicopter rotor testing.
Notes: Distributed to depository libraries in microfiche.

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