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Effects of Convoluted Divergent Flap Contouring on the Performance of a Fixed-Geometry Nonaxisymmetric Exhaust Nozzle [microform]

Scott C. Asbury and Craig A. Hunter
Format
Book; Government Document; Microform
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
Language
English
Series
NASA/TP
NASA Technical Paper
SuDoc Number
NAS 1.60:209093
Description
1 v.
Notes
Shipping list no.: 99-0723-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.
Series Statement
NASA/TP ; 1999-209093
NASA technical paper 209093
Technical Details
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    a| 2
    650
      
    7
    a| Convergent-divergent nozzles. 2| nasat
    650
      
    7
    a| Boundary layer separation. 2| nasat
    650
      
    7
    a| Wind tunnel nozzles. 2| nasat
    650
      
    7
    a| Wind tunnel tests. 2| nasat
    650
      
    7
    a| Nozzle flow. 2| nasat
    650
      
    7
    a| Oblique shock waves. 2| nasat
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    a| Flow visualization. 2| nasat
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