Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊/

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Bibliographic Details
Main 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, February 1985.
Series:NASA technical paper ; 2391.
Subjects:
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513 |a Technical paper. 
588 |a Description based on online resource, PDF version; title from title page (NASA, viewed Aug. 23, 2018). 
650 7 |a Convergent.  |2 nasat 
650 7 |a Thrust vector control.  |2 nasat 
650 7 |a Wind tunnel tests.  |2 nasat 
650 7 |a Nozzle flow.  |2 nasat 
650 7 |a Transonic wind tunnels.  |2 nasat 
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710 2 |a Langley Research Center. 
776 0 8 |i Microfiche version:  |a Leavitt, Laurence D.  |t Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60°.  |d [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985  |w (OCoLC)56497170 
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