Unsteady flows in a single-stage transonic axial-flow fan stator row

Unsteady flows in a single-stage transonic axial-flow fan stator row [microform] / Michael D. Hathaway.

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Bibliographic Details
Main Author: Hathaway, Michael D.
Corporate Authors: United States. National Aeronautics and Space Administration, United States. Army Aviation Systems Command
Other title:Unsteady flows in a single stage transonic axial-flow fan stator row.
Format: Government Document Microfilm Book
Language:English
Published: [Washington, D.C.] : [St. Louis, MO] : [Springfield, Va.] : National Aeronautics and Space Administration ; U.S. Army Aviation Systems Command ; [For sale by the National Technical Information Service], [1986]
Series:NASA technical memorandum ; 88929.
AVSCOM technical report ; 86-C-29.
Subjects:
Unsteady flow (Aerodynamics) > Measurement.
Turbomachines > Performance.
Axial flow turbines.
Stator blades.
Transonic flow.
Turbocompressors.
Turbo engines.
Unsteady flow.
Description
Item Description:Cover title.
Distributed to depository libraries in microfiche.
"December 1986."
Physical Description:vii, 200 pages : illustrations ; 28 cm.
Bibliography:Includes bibliographical references (pages 145-156)

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