Wind Tunnel Tests on Projectile Models in 0 .3M Trisonic Wind Tunnel

Krishnamurthy, K (1989) Wind Tunnel Tests on Projectile Models in 0 .3M Trisonic Wind Tunnel. Technical Report. NAL, Bangalore.

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    Abstract

    This Document Gives The Results Of Tests Conducted For The Armament Research And Development Establishment, Pune On 2/5th Scale Models Of Two Modified Projectiles In The 0 .3M X 0.3M Trisonic Wind Tunnel Of The National Aeronautical Laboratory, Bangalore . The Models Designated As Projectile I And Projectile II Were Tested In The Mach Number Range Of 0 .6 To 3.0. Angle Of Attack Range Of -4 0 To +150 Was Covered In Steps Of 20 . The Forces And Moments On The Models Were Measured Using A Six Component Internal Strain Gauge Balance. Schlieren Photographs Were Also Taken To Study The Shock Wave Pattern On The Models.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Wind Tunnel Tests; Projectiles
    Subjects: AERONAUTICS > Aeronautics (General)
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 31 Oct 2012 09:51
    Last Modified: 31 Oct 2012 09:51
    URI: http://nal-ir.nal.res.in/id/eprint/11324

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