Missile Aerodynamics Design Manual

Anon, - (1987) Missile Aerodynamics Design Manual. Project Report. NAL, Bangalore.

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    Abstract

    This proposal describes the first phase of the work comtemplated for the Missile Design Manual . The project envisages to undertake the development of a Computer Code for the estimation of Six-component forces and moments for nonzero roll orientations of wing-body-tail Cruciform Configuration. It includes experimental study of the effects of nose-bluntness, midbody/aftbody flare and boattail, and also of the control-surface gap on the aerodynamic characteristics of axisymmetric bodies, and incorporation of these effects ih the main code.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Missiles;Slender bodies;Cruciform bodies
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: Mr Nisanth
    Date Deposited: 25 Jul 2012 11:56
    Last Modified: 25 Jul 2012 11:56
    URI: http://nal-ir.nal.res.in/id/eprint/10616

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