Varute, PT and Eashwar, T and Srinivasa, A and Balakrishna, S (1976) Development of quick acting valve for plot hypersonic wind tunnel of Indian Institute of Science, Bangalore. Technical Report. National Aeronautical Laboratory, Bangalore, India.
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Abstract
An automatically operated quick opening and closing valve installedat the critical location in the tunnel circuit is an essential component of the hypersonic tunnel. The primary function of the valve is isolate the air mass flow to the shut off rapidly and test section; Fig.3 valve Q3. a blow off valve by rapidly the atmosphere; Fig. 3 valve In some instances it may act as opening the pressurized area to Q2 and Q4.
Item Type: | Monograph (Technical Report) |
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Uncontrolled Keywords: | Pilot hypersonic wind tunnel;Hydraulic system design |
Subjects: | AERONAUTICS > Aerodynamics |
Depositing User: | M/S ICAST NAL |
Date Deposited: | 12 Sep 2006 |
Last Modified: | 24 May 2010 04:20 |
URI: | http://nal-ir.nal.res.in/id/eprint/2681 |
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