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of the suction surface between the throat and the trailing edge is called the "region of
suction surface, and lower on the less-curved pressure surface.
in this case the maximum velocity on the suction surface occurs a little downstream of the
High-efficiency turbine geometries would exhibit continuously accelerating flow on the suction surface up to the maximum velocity near the throat, and then minimum deceleration (minimum diffusion) from there to the trailing edge.
due to blending of a leading-edge circle with the blade suction surface occurs in the
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