Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance
By: Steven R. Wellborn and Theodore H. Okiishi.
Contributors: Okiishi, T. H. 1939-; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- 198536.; NASA contractor report -- NASA CR-198536.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Turbomachinery.; Turbocompressors.; Stator blades.; Rotors.; Losses.; Flow distribution.; Degradation.; Aerodynamic characteristics.
Notes: Shipping list no.: 98-0452-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 2 microfiches.