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A similarity rule for compressibility and sidewall-boundary-layer effects in two-dimensional wind tunnels
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1979
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Two-dimensional Wind TunnelsAeroacousticsUnsteady FlowCompressible FlowEngineeringSimilarity RuleSidewall Momentum IntegralSidewall Boundary LayerSidewall SuctionFluid MechanicsCivil EngineeringTurbulence ModelingIncompressible FlowFlow PhysicAerodynamicsSidewall-boundary-layer EffectsWind EngineeringBoundary Layer
The effect of the sidewall boundary layer on flow in two-dimensional wind tunnels is determined. The small-disturbance and isentropic approximations are made, and the sidewall-boundary-layer dynamics are modeled with the von Karman momentum-integral equation. The effects of the edge-velocity-gradient term in the sidewall momentum integral, which is usually dominant near the model, and the compressibility term are shown to be similar. It is shown that the effect of sidewall suction around the model is not similar to two-dimensional flow. Comparisons with experiment are made to verify the similarity rule.