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Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60°
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degrees
National Aeronautics and Space Administration.
Scientific and Technical Information Branch,
1 online resource (141 pages) : illustrations.
Bobby L. Berrier and Laurence D. Leavitt.
"October 1984"--Report documentation page.
"Performing organization: NASA Langley Research Center"--Report documentation page.
Includes bibliographical references (page 11).
National Aeronautics and Space Administration 505-43-90-07 L-15766
Static internal performance of single-expansion-ramp nozzles with thrust-vectoring capability up to 60°