An Experimental Study On The Aerodynamic Effects Of Flare On An Axisymmetric Body

Umakant, J and Krishnamurthy, M (1993) An Experimental Study On The Aerodynamic Effects Of Flare On An Axisymmetric Body. Technical Report. NAL, Bangalore.

Full text available as:
[img] PDF
Download (62Kb)

    Abstract

    A Systematic Study Has Been Undertaken To Investigate The Effects Of Flare On An Axisymmetric Body, Typical Of Missile Configurations . Measurements Have Been Made Of The Longitudinal Aerodynamic Characteristics Of The Model For Angles Of Attack Upto 20 Deg . And Mach Numbers Ranging From 0.5 To 3.0. Flares Of Angles 5° , 10 ° , 15° And 20° At Three Axial Positions Have Been Considered In The Study. Test Results Have Been Presented In The Form Of Tables And Aerodynamic Characteristic Plots For Typical Subsonic, Transonic And Supersonic Mach Numbers Are Included .

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Aerodynamic characteristics; flare; Axisymmetric body
    Subjects: ASTRONAUTICS > Astronautics (General)
    Division/Department: Experimental Aerodynamics Division, Experimental Aerodynamics Division
    Depositing User: M/S ICAST NAL
    Date Deposited: 08 Aug 2012 15:30
    Last Modified: 08 Aug 2012 15:30
    URI: http://nal-ir.nal.res.in/id/eprint/10770

    Actions (login required)

    View Item