Aerodynamic design of two dimensional supersonic nozzle contours with boundary layer corrections

Satyanarayana, B and Irani, PA (1961) Aerodynamic design of two dimensional supersonic nozzle contours with boundary layer corrections. Technical Report. National Aeronautical Laboratory, Bangalore,India.

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    Abstract

    Various methods of determining supersonic aerodynamic nozzle contours are presented. The aerodynamic contours their slcpes and curvatures are calculated both by the graphical as well as Poelsch's methods. The displacement thickness Is determined on the side walls and contour waiis and the aerodyiiaxic contours corrected for boundary layeyer effects are presented.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Supersonic;Aerodynamic nozzle;Poelsch's methods
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 19 Dec 2006
    Last Modified: 24 May 2010 09:54
    URI: http://nal-ir.nal.res.in/id/eprint/3781

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