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Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° / Bobby L. Berrier and Laurence D. Leavitt.

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Format:
Book
Government document
Author/Creator:
Berrier, Bobby L., author.
Leavitt, Laurence D., author.
Contributor:
Langley Research Center
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Series:
NASA technical paper ; 2364.
NASA technical paper ; 2364
Language:
English
Subjects (All):
Transonic wind tunnels.
Genre:
Online resources.
Physical Description:
1 online resource (141 pages) : illustrations
Other Title:
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degrees
Place of Publication:
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1984.
Notes:
"October 1984"--Report documentation page
"Performing organization: NASA Langley Research Center"--Report documentation page
Includes bibliographical references (page 11).
Online resource; title from PDF title page (NASA, viewed January 26, 2017).
Other Format:
Microfiche version: Berrier, Bobby L. Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60°
OCLC:
970166733

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