Design of nozzle for tunnel which operates between limits Mach number 1.0 to Mach number 2.0; in arriving at solution, aerodynamic as well as mechanical phases of problem are considered. Bibliography. Thesis Submitted to Case School of Applied Science in Partial Fulfillment of Requirements for Degree of Master of Science in Mechanical Engineering.


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    Titel :

    Design of variable-throat rectangular nozzle for supersonic wind tunnel


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Publ


    Beteiligte:
    Shaffer, B.W. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    68 pages


    Anmerkungen:

    20 Supp sheets


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Variable Throat Nozzle

    S. L. Hardy | NTIS | 1965


    Variable Throat Nozzle

    W. B. Wilson | NTIS | 1965



    Nozzle Throat Optimization for Supersonic Jet Noise Reduction

    Gustafsson, B. / Cuppoletti, D. / Gutmark, E. et al. | British Library Conference Proceedings | 2012


    Nozzle throat optimization for supersonic jet noise reduction

    Gustafsson, Bernhard / Cuppoletti, Daniel / Gutmark, Ephraim et al. | AIAA | 2012