Experimental Studies on a 1/12 Scale Model of Prithvi Missile

Kanagarajan, V and Arokkiaswamy, A (1986) Experimental Studies on a 1/12 Scale Model of Prithvi Missile. Project Report. NAL, Bangalore.

Full text available as:
[img] PDF
Download (58Kb)


    Wind Tunnel Tests were carried out to determine the Longitudinal. static stability and roll control characteristics of a 1/12 scale 'PRITHVI' missile configuration with cruciform trapezoidal wings and aft tail fin controls . The tests were conducted ih the 1 .2m Trisonic wind tunnel at Mach numbers from 0 .4 to 1 .5 through an angle of attack range of -10° to 20° . Model roll orientation was varied from -45° to 45 ° . The results indicated good longitudinal stability characteristics throughout the test Mach number range .

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Missile;Cruciform;Tail Control;Wing-Body-Tail
    Subjects: AERONAUTICS > Aerodynamics
    AERONAUTICS > Aircraft Design, Testing & Performance
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: Mr Nisanth
    Date Deposited: 18 Jul 2012 13:27
    Last Modified: 18 Jul 2012 13:27
    URI: http://nal-ir.nal.res.in/id/eprint/10558

    Actions (login required)

    View Item