Contour corrections, small in comparison with boundary-layer thickness, produce flow changes which cannot be adequately described by simple theory of characteristics; procedure involving use of experimentally determined jack influences was successfully applied to correction of nozzle profiles in 12-in. supersonic wind tunnel; considerations of further application of this method.


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    Titel :

    Correction of flexible plate supersonic nozzle contours by influence methods


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1955


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Flexible nozzle for small supersonic wind tunnel

    Dhawan, S. / Roshko, A. | Engineering Index Backfile | 1951


    Investigation of a Single-Jack Flexible Supersonic Nozzle

    Juhany, Khalid / Husini, Husam | AIAA | 2007



    Design of Maximum Thrust Nozzle Contours by Direct Optimization Methods

    Jeffrey G. Allman / Joe D. Hoffman | AIAA | 1981