Report presents combined analytical and experimental approach to investigation of external aerodynamic performance of supersonic airplane-nozzle systems at subsonic speeds; experimental techniques are described which can minimize model scaling uncertainties in wind-tunnel tests; analysis method for successfully predicting drag on axisymmetric bodies at subsonic speeds combines axisymmetric potential flowfield predictions with laminar and turbulent boundary-layer computation procedures; results for certain applications are compared with experiment, and application of analysis to design of asymmetric models is demonstrated.


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    Titel :

    Subsonic aerodynamic performance of nozzle installations in supersonic airplanes


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Armstrong, R.S. (Autor:in) / Miller, S.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch







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