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The Maximum Pressure Rise Attainable in Subsonic Diffusers
Published online by Cambridge University Press: 04 July 2016
Summary
An analysis of experimental results shows that the maximum pressure rise attainable in a two-dimensional subsonic diffuser of length L correlates with the parameter L/δ0*, δ0* being the displacement thickness of the boundary layer at entry. The results agree well with boundary layer theory.
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- Copyright © Royal Aeronautical Society 1965
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