Quantitative pressure and force data for five axisymmetric boattail nozzle configurations were examined. These configurations simulate the variable-geometry feature of a single nozzle design operating over a range of engine operating conditions. Five nozzles were tested in the Langley 16-Foot Transonic Tunnel at Mach numbers from 0.60 to 1.30. The experimental data were also compared with theoretical predictions.


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    Titel :

    Experimental and Analytical Investigation of Axisymmetric Supersonic Cruise Nozzle Geometry at Mach Numbers from 0.60 to 1.30


    Beteiligte:
    G. T. Carson (Autor:in) / E. E. Lee (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    89 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch