High Speed Wind Tunnel Tests of Some Turbine Blades

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  • タービン翼の高速翼列実験
  • タービンヨク ノ コウソクヨクレツ ジッケン

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Abstract

This report presents the results of high speed cascade tests for some turbine blades. The wind tunnel used for the cascade test had the test section at the suction side of blower, and the control of the boundary layer at the side wall was ignored for the sake of simplicity. One typical impulse blade and also one nozzle profile were tested, and the effects of pitch-chord ratio were mainly investigated.

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