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Author
Berrier, Bobby L., author.
Title
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° / Bobby L. Berrier and Laurence D. Leavitt.
Publication Info.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1984.
Connect to
Connect to http://purl.fdlp.gov/GPO/gpo76455
Copies
Location
Call No.
OPAC Message
Status
Axe Federal Documents Online
NAS 1.60:2364
---
Available
Description
1 online resource (141 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series
NASA technical paper ; 2364
NASA technical paper ; 2364.
Note
"October 1984"—Report documentation page.
"Performing organization: NASA Langley Research Center"—Report documentation page.
Bibliography
Includes bibliographical references (page 11).
Type Of Report
Technical paper.
Funding
National Aeronautics and Space Administration 505-43-90-07 L-15766
Note
Description based on online resource; title from PDF title page (NASA, viewed Jan. 26, 2017).
Subject
Axisymmetric bodies .
Nozzle thrust coefficients .
Static tests .
Thrust vector control .
Transonic wind tunnels .
Two dimensional flow .
Genre/Form
Online resources.
Added Author
Leavitt, Laurence D., author.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Added Title
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degrees
Other Form:
Microfiche version: Berrier, Bobby L. Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60° (OCoLC)22257163
Gpo Item No.
0830-H-15 (online)
Sudoc No.
NAS 1.60:2364
Available items only
