The design and cascade tests of free-streamline and full-contour 160 degrees turning supersonic-turbine-blade sections
Description: Report presenting a study of the flow characteristics of two supersonic-impulse-turbine-blade sections designed for a turning angle of 160 degrees. The primary difference between the two sections was the cutting away of a large portion of the convex surface and the presence of a free streamline as the boundary of flow in the passage. Results regarding the full-contour blade, free-streamline blade, and a comparison of the two are provided.
Date: August 16, 1957
Creator: Westphal, Willard R.
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Partner: UNT Libraries Government Documents Department