Pressure sweep generator for the NAL 4-ft trisonic wind tunnel

Narayan, G and Mahalingam, V and Srikantan, KV (1975) Pressure sweep generator for the NAL 4-ft trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    For efficient testing of aeroelastic models in wind tunnels, a programmed variation of the dynamic pressure during a run is desirable. A system which provides variation of dynamic pressure resulting from a variation of stagnation pressure, in either a step-mode or a continuous mode has been designed and integrated with the PRV control systems of the HAL 4-ft trisonic wind tunnel. This report describes the salient features of the system and provides its operating instructions.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Trisonic wind tunnel;Generator
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics, Aerodynamics, Aerodynamics
    Depositing User: Mr. Ravikumar R
    Date Deposited: 31 Aug 2006
    Last Modified: 24 May 2010 09:50

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