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.
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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 |
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