Suryanarayana, BG (1974) Design of a sidewall mounted model injection system for the NAL 1x2019; x 1x2019; trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
This report describes the design features of the injection-system for testing Aeroelastic and flutter models mounted in the sidewall of the NAL 1' X 1' Trisonic Wind Tunnel. Heat transfer and dynamic stability studies on models can also be made by utilising this facility. The experience13; gained in the design and operation of this system would be a valuable guide in designing a similar facility for the NAL 4' X 4' trisonic wind tunnel.
Item Type: | Monograph (Technical Report) |
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Uncontrolled Keywords: | Trisonic wind tunnel;Injection system |
Subjects: | AERONAUTICS > Aerodynamics |
Depositing User: | Mr. Ravikumar R |
Date Deposited: | 31 Aug 2006 |
Last Modified: | 24 May 2010 04:20 |
URI: | http://nal-ir.nal.res.in/id/eprint/2612 |
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