Development of pressure regulating valve for cascade tunnel

Varute, PT and Samraj, AC (1974) Development of pressure regulating valve for cascade tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Full text available as:
[img] PDF
Restricted to Archive staff only

Download (1440Kb)


    An automatically controlled Pressure Regulating Valve13; located between the air receivers and the settling chamber of the tunnel is an essential component for the purpose of13; maintaining the stagnation pressure in the settling chamber13; at a predetermined value during a test run.13; Development of a Pressure Regulating Valve (P.R.V)13; including its hydraulic system for Propulsion Division of N.A.L. was undertaken by Instrumentation Division. The absolute necessity of a P.R.V. for the proposed Transonic Cascade Tunnel, the non-availability of free foreign exchange for its procurement from abroad, non-availability of such a unit readily in the indigenous market, was the motivation for the development of a suitable unit within N.A.L.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Cascade tunnel;Valve
    Subjects: AERONAUTICS > Aircraft Propulsion and Power
    Division/Department: Propulsion Division, Propulsion Division
    Depositing User: Mr. Ravikumar R
    Date Deposited: 29 Nov 2006
    Last Modified: 24 May 2010 09:53

    Actions (login required)

    View Item