Experimental and computational investigation of the tip clearance flow in a transonic axial compressor rotor
By: Kenneth L. Suder and Mark L. Celestina.
Contributors: Celestina, Mark L.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 106711.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airspeed.; Applications programs (Computers); Blade tips.; Blade-vortex interaction.; Compressor rotors.; Laser anemometers.; Shock wave interaction.; Tip speed.; Transonic compressors.; Turbo compressors.; Vortices.; Wall flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0021-M.

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