Axisymetric supersonic nozzle design foelsch method

Desai, SS (1977) Axisymetric supersonic nozzle design foelsch method. Technical Report. National Aeronautical Laboratory, Bangalore,India.

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    A computer programme is given here for the calculation of13; axisymmetric supersonic nozzles for use in aerodynamic test13; facilities The approximate method due to Foelsch is adopted.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: calculation of axisymmetric supersonic nozzles;Aerodynamic test
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 14 Sep 2006
    Last Modified: 24 May 2010 09:50

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