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: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Trisonic wind tunnel;Injection system |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 31 Aug 2006 |
| Last Modified: | 24 May 2010 09:50 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2612 |
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