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Publish Date
1995
Publisher
National Aeronautics and Space Administration, Langley Research Center,
Available from the National Technical Information Service
Language
English
Pages
209
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Subjects
Jet nozzles, Aerodynamic loadShowing 1 featured edition. View all 1 editions?
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Afterbody/nozzle pressure distributions of a twin-tail twin-enginer fighter with axisymmetric nozzles at Mach numbers from 0.6 to 1.2
1995, National Aeronautics and Space Administration, Langley Research Center, Available from the National Technical Information Service
in English
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Book Details
Edition Notes
"May 1995."
"Performing organization report number L-17438"--Report documentation page.
Includes bibliographical references (p. 10).
Available electronically at the following URL address: http://techreports.larc.nasa.gov/ltrs/ltrs.html.
WU 505-59-30-04.
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- Created September 27, 2008
- 3 revisions
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