Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° /

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Bibliographic Details
Main Authors: Berrier, Bobby L. (Author), Leavitt, Laurence D. (Author)
Corporate Author: Langley Research Center.
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1984.
Series:NASA technical paper ; 2364.
Subjects:
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246 3 |a Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degrees 
264 1 |a [Washington, D.C.] :  |b National Aeronautics and Space Administration, Scientific and Technical Information Branch,  |c October 1984. 
300 |a 1 online resource (141 pages) :  |b illustrations. 
336 |a text  |b txt  |2 rdacontent 
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500 |a "October 1984"--Report documentation page. 
500 |a "Performing organization: NASA Langley Research Center"--Report documentation page. 
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513 |a Technical paper. 
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588 |a Description based on online resource; title from PDF title page (NASA, viewed Jan. 26, 2017). 
650 7 |a Axisymmetric bodies.  |2 nasat 
650 7 |a Nozzle thrust coefficients.  |2 nasat 
650 7 |a Static tests.  |2 nasat 
650 7 |a Thrust vector control.  |2 nasat 
650 7 |a Transonic wind tunnels.  |2 nasat 
650 7 |a Two dimensional flow.  |2 nasat 
700 1 |a Leavitt, Laurence D.,  |e author. 
710 2 |a Langley Research Center. 
710 1 |a United States.  |b National Aeronautics and Space Administration.  |b Scientific and Technical Information Branch,  |e issuing body. 
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