Effects of inlet distortion on the development of secondary flows in a subsonic axial inlet compressor rotor
By: Albert K. Owen.
Contributors: United States. Army Aviation Research and Technology Activity.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 104356.; AVSCOM technical report -- 90-C-012.; AVSCOM technical report -- 90-C-12.
Publisher: National Aeronautics and Space Administration; US Army Aviation Systems Command, Aviation R&T Activity; For sale by the National Technical information Service
Published: 1991
Place of publication: [Washington, DC]; [St. Louis, Mo.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Turbine-propeller engines.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1991. 4 microfiches.