Vinay Kumar, - (1989) Experimental studies on a 1/10th scale model of Agni- payload missile. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
Wind tunnel tests were carried out to determine the aerodynamic characteristics of a 1/10th scale AGNI-payload, missile model. The tests were conducted in the NAL 1.2M Trisonic Wind Tunnel at Mach numbers from 0.5 to 4.0 through an angle of attack range of -5
| Item Type: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | AGNI-Payload;Missiles |
| Subjects: | AERONAUTICS > Aerodynamics |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 19 Dec 2012 04:39 |
| Last Modified: | 19 Dec 2012 04:39 |
| URI: | http://nal-ir.nal.res.in/id/eprint/11395 |
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