Unsteady flows in a single-stage transonic axial-flow fan stator row
By: Michael D. Hathaway.
Contributors: United States. National Aeronautics and Space Administration.; United States. Army Aviation Systems Command.
Series: NASA technical memorandum -- 88929.; USAAVSCOM technical report -- 86-C-29.; AVSCOM technical report -- 86-C-29.
Publisher: National Aeronautics and Space Administration; U.S. Army Aviation Systems Command; For sale by the National Technical Information Service
Published: 1986
Place of publication: [Washington, D.C.]; [St. Louis, MO]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 200
Subjects: Unsteady flow (Aerodynamics) -- Measurement.; Turbomachines -- Performance.; Axial flow turbines.; Stator blades.; Transonic flow.; Turbocompressors.; Turbo engines.; Unsteady flow.
Other titles: Unsteady flows in a single stage transonic axial-flow fan stator row.
Notes: Cover title.

Distributed to depository libraries in microfiche.

"December 1986."

Includes bibliographical references (p. 145-156).

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1987] 3 microfiches ; negative.