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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    Title :

    Design of variable-throat rectangular nozzle for supersonic wind tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Publ


    Contributors:


    Publication date :

    1947


    Size :

    68 pages


    Remarks:

    20 Supp sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Variable Throat Nozzle

    S. L. Hardy | NTIS | 1965


    Variable Throat Nozzle

    W. B. Wilson | NTIS | 1965



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