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Transitional Boundary Layers under the Influence of High Free Stream Turbulence,Intensive Wall Cooling and High Pressure Gradients in Hot Gas Circulation.

机译:高自由流湍流,强壁冷却和高压梯度对热气体循环影响的过渡边界层。

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摘要

The requirements for fundamental experimental studies of the influence of free stream turbulence, pressure gradients and wall cooling are discussed. Under turbine-like free stream conditions, comprehensive tests of transitional boundary layers with laminar, reversing and turbulent flow increments were performed to decouple the effects of the parameters and to determine the effects during mutual interaction.

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