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:

MARC

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246 2 |a Unsteady flows in a single stage transonic axial-flow fan stator row. 
260 |a [Washington, D.C.] :  |b National Aeronautics and Space Administration ;  |a [St. Louis, MO] :  |b U.S. Army Aviation Systems Command ;  |a [Springfield, Va.] :  |b [For sale by the National Technical Information Service],  |c [1986] 
300 |a vii, 200 pages :  |b illustrations ;  |c 28 cm. 
336 |a text  |b txt  |2 rdacontent. 
337 |a microform  |b h  |2 rdamedia. 
338 |a microfiche  |b he  |2 rdacarrier. 
490 1 |a NASA technical memorandum ;  |v 88929. 
490 1 |a AVSCOM technical report ;  |v 86-C-29. 
500 |a Cover title. 
500 |a Distributed to depository libraries in microfiche. 
500 |a "December 1986." 
504 |a Includes bibliographical references (pages 145-156) 
533 |a Microfiche.  |b [Washington, D.C. :  |c National Aeronautics and Space Administration,  |d 1987]  |e 3 microfiches ; negative. 
539 |a s  |b 1987  |d dcu  |e n. 
650 0 |a Unsteady flow (Aerodynamics)  |x Measurement. 
650 0 |a Turbomachines  |x Performance.  |0 http://id.loc.gov/authorities/subjects/sh85138750. 
650 7 |a Axial flow turbines.  |2 nasat. 
650 7 |a Stator blades.  |2 nasat. 
650 7 |a Transonic flow.  |2 nasat. 
650 7 |a Turbocompressors.  |2 nasat. 
650 7 |a Turbo engines.  |2 nasat. 
650 7 |a Unsteady flow.  |2 nasat. 
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