Prediction Of Drag Of Missiles At Subsonic, Transonic And Supersonic Speeds

Seshadri, SN (1993) Prediction Of Drag Of Missiles At Subsonic, Transonic And Supersonic Speeds. Technical Report. NAL, Bangalore.

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    Abstract

    A Computer Code Has Been Developed To Predict The Drag Characteristics Of Missile Configurations At Subsonic, Transonic And Supersonic Speeds And Is Based On Semi-Empirical Methods . The Method' Handles Complex Configurations (Wing, Body, Tail, Canard) And Is Valid Upto High Angles Of Attack . The Code Has Been Validated Against A Large Number Of Experimental Results Particularly At Supersonic Speeds . The Agreement Between Prediction And Experiment Is Very Good . Validation At Subsonic And Transonic Speeds Is In Progress .

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Missile Drag; Drag Characteristics
    Subjects: ASTRONAUTICS > Astronautics (General)
    Division/Department: 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/10766

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