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+91 98967 93832Enables the user to carry out advanced studies in the Aerodynamics fields. These include boundary layer experiments, flow visualisation, pressure distribution, study of turbulence and offer the possibility of developing self-design aerodynamics profiles to be tested.
A stand-alone computer controlled subsonic wind tunnel for conducting experiments in aerodynamics including boundary layer experiments, flow visualisation, pressure distribution, study of turbulence and offering the possibility of developing self-design aerodynamics profiles to be tested.
































