Pressure measurements in the heat shield region of 1/80 scale PSLV model In the mach number range of 0.8 to 4.0

Sajeer, Ahmed and Selvarajan, S (1985) Pressure measurements in the heat shield region of 1/80 scale PSLV model In the mach number range of 0.8 to 4.0. Project Report. National Aerospace Laboratories, Bangalore.

Full text available as:
[img] PDF
Download (62Kb)

    Abstract

    Pressure measurements were carried out in the heatshield region of a 1/80 scale PSLV pressure model in the Mach number range of 0.8 to 4.0 and at incidences of 0 and 5 degrees in the 1.2M tunnel to supplement the pressure data obtained in 0.3M tunnel where tests on the model covered transonic Mach numbers only and also to have a comparison of the pressure data with that of 0.3M tunnel for any tunnel/support system interference. Results show a good comparison of the pressures with respect to those of 0.3M tunnel at M=0.78.

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: PSLV;Steady pressure;Heat shield region
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics
    Depositing User: Smt Bhagya Rekha KA
    Date Deposited: 26 Sep 2012 14:09
    Last Modified: 26 Sep 2012 14:09
    URI: http://nal-ir.nal.res.in/id/eprint/11028

    Actions (login required)

    View Item