Slope and deflection of 4-FT.Tunnel model support stings

Desikan, KS (1972) Slope and deflection of 4-FT.Tunnel model support stings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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Abstract

The models for force and pressure measurements in 4-ft. Trisonic Wind Tunnel are generally mounted on stings. For pressure measurements, the model is directly secured on to the sting and for force measurements, the model is supported via a balance mounted on the stings.13;

Item Type: Monograph (Technical Report)
Uncontrolled Keywords: Trisonic wind tunnel;Pressure measurements
Subjects: AERONAUTICS > Aerodynamics
Depositing User: M/S ICAST NAL
Date Deposited: 10 Nov 2006
Last Modified: 24 May 2010 04:23
URI: http://nal-ir.nal.res.in/id/eprint/3345

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