Formal force characteristics of cone-cylinder and ogive cylinder bodies at mach number = 1.8

Shanbhag, VV and Rao, RU (1970) Formal force characteristics of cone-cylinder and ogive cylinder bodies at mach number = 1.8. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Full text available as:
[img] PDF
Restricted to Archive staff only

Download (204Kb)

    Abstract

    An investigation has been conducted in 1 ' x 1 ' trisonic tunnel of National Aeronautical Laboratory to determine aerodynamic characteristics of cone-cylinder and ogive cylinder bodies of nose fineness ratios of three, five and seven for angles of attack 0xB0; to 5xB0;? the afterbody fineness ratio being ten for all the models. 13; The results indicate . that the normal force is slightly higher for ogive cylinder body than cone-cylinder body of nose fineness ratio 3, and lower than cone-cylinder body for nose fineness ratio 7, and there is crossing of curves for nose fineness ratio equal to 5. This interesting phenomenon requires further investigation.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Rockets;Upper atmosphere;Aerodynamic;Transonic speeds;Lower supersonic speeds
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 19 Dec 2006
    Last Modified: 24 May 2010 09:54
    URI: http://nal-ir.nal.res.in/id/eprint/3688

    Actions (login required)

    View Item