Tests On Various Nose Configurations With Cylindrical After body In 0.3m Wind Tunnel.

Krishnamurthy, K (1989) Tests On Various Nose Configurations With Cylindrical After body In 0.3m Wind Tunnel. Technical Report. NAL, Bangalore.

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    Abstract

    Force Measurements On Four Nose Configurations With Cylindrical After body Were Performed In 0.3m Wind Tunnel In The Mach Number Range Of 0.5 To 0.8 And Angle Of Incidence -4 To 14°.From Analysis Of Aerodynamic Data, It Was Observed That The Bulbous Nose Configuration Was The Optimum Configuration With Drag Penalty.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Nose configurations; After body; Mach number; Force - measurements.
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 27 Nov 2012 09:53
    Last Modified: 27 Nov 2012 09:53
    URI: http://nal-ir.nal.res.in/id/eprint/11342

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