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Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude

Author: David M Straight; Richard R Cullom; Lewis Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Publisher: Washington D.C. : National Aeronautics and Space Administration Scieentific and Technical Information Branch ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1983.
Series: NASA technical paper, 2171.
Edition/Format:   Print book : National government publication : EnglishView all editions and formats
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Additional Physical Format: Online version:
Straight, David M.
Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude.
Washington D.C. : National Aeronautics and Space Administration Scieentific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983
(OCoLC)761364881
Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: David M Straight; Richard R Cullom; Lewis Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
OCLC Number: 10494363
Notes: "Lewis Research Center."
Distributed to depository libraries in microfiche.
"June 1983"--Cover.
STAR category 07.
Description: 36 pages : illustrations ; 28 cm.
Series Title: NASA technical paper, 2171.
Responsibility: David M. Straight and Richard R. Cullom.

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