Aerodynamic design of a variable mach number supersonic nozzle for the 4'X4' trisonic tunnel

Acharya, YVG (1961) Aerodynamic design of a variable mach number supersonic nozzle for the 4'X4' trisonic tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    The methods available for designing supersonic nozzles have been described briefly. The methods, which are considered suitable for designing the variable Mach number nozzle have been discussed in more detail. Examples of the design of the nozzle contour for a particular Mach number by the recommended methods are given.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Supersonic nozzles;Aerodynamic design;Trisonic tunnel
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 19 Jan 2007
    Last Modified: 24 May 2010 09:54
    URI: http://nal-ir.nal.res.in/id/eprint/3774

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