Design data are presented for the graphical construction of two-dimensional sharp-edge-throat supersonic nozzles of minimum length for test-section Mach numbers from 1.20 to 10.00. The method of characteristics used in the design is briefly reviewed.


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    Title :

    Design Data for Graphical Construction of Two-Dimensional Sharp-Edge-Throat Supersonic Nozzles


    Contributors:
    H. Shames (author) / F. L. Seashore (author)

    Publication date :

    1948


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English