Selvarajan, S and Arokkiaswamy, A and Kanagarajan, V (1988) Wind Tunnel Force Measurements on 1/12 Scale Model of PRITHVI missile Configuration - II : Final Report. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
This report presents the aerodynamic data generated on a 1/12 scale model of PRITHVI missile configuration - II through tests in the NAL 1.2m wind tunnel. The tests were carried out to obtain aerodynamic data to determine the control effectiveness characteristics of the tail fin Controlled missile model. The presentation of test results include the following : (i) basic tests (without CDS) and roll effectiveness tests at M=0.4 to 1.2 (ii) Pitch and yaw effectiveness tests in the Mach number range 1.5 to 3.5 (iii) Effect of protrusions on the basic configuration. The test Reynolds number based on the body diameter varied from 1.1 million to 2.8 million. Complete test results are given in the form of tables with few typical plots.
| Item Type: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | Force measurements;Prithvi configuration |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 03 Sep 2012 08:10 |
| Last Modified: | 03 Sep 2012 08:10 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10881 |
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