Balakrishna, S and Niranjana, T and Rajan, SR (1991) Augmentation of the 1.2m x 1.2m low speed dynamic test wind tunnel at NAL. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
This document details the Augmentation of the 1.2m x l.2m13; Low speed Dynamic Test Wind Tunnel at Flight Mechanics amp; Controls Division. The Tunnel designed in 1982 was originally capable of 32 m/s fixed speed. With sponsorship of AR amp; DB, the tunnel volocity has been enhanced to variable speed capability of 20-60 m/s using a 175 kw DC motor and an inlet Guide Vane system capable of 1:1:8 ratio speed control. The latter provides 5 m/s/s flow acceleration capability. This ARDB project has been completed in 15 months time
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Inlet guide vane;Tunnel velocity control |
| Subjects: | AERONAUTICS > Aircraft Stability and Control |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | Mr. Ravikumar R |
| Date Deposited: | 18 Jul 2006 |
| Last Modified: | 24 May 2010 09:43 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1790 |
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