Programs to analyze supersonic flow past right circular cones with a view to make use of uncalibrated cones for determination of flow angles and mach numbers in wind tunnels

Viswanathan, S (1970) Programs to analyze supersonic flow past right circular cones with a view to make use of uncalibrated cones for determination of flow angles and mach numbers in wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    Two programs are developed for SIRIUS Digital computer to13; analyse the supersonic flow around right circular cones at zero angle of attack and at small angle of attack. These programs can be used 1;0 generate tables similar to NASA SP-3004 (Ref.1) and NASA SP-3007( Ref.2). Certain modif1cations are incorporated in the programs to make use of13; the same to calibrate any wind tunnel in supersonic range for local flow inclination and free stream Mach number using an uncalibrated conical pressure probe,

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: SIRIUS digital computer;Trisonic wind tunnel
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 10 Nov 2006
    Last Modified: 24 May 2010 09:53
    URI: http://nal-ir.nal.res.in/id/eprint/3343

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