Process to minimize turbine airfoil downstream shock induced flowfield disturbance

A process of designing a transonic airfoil that results in an exit deviation angle that is optimized to minimize downstream shock induced flowfield disturbances. Specifically, a design process of a transonic airfoil minimizes pitchwise variation in downstream static pressure that includes determinin...

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1. Verfasser:	McKeever, Craig W
Format:	Patent
Sprache:	eng
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creator	McKeever, Craig W
description	A process of designing a transonic airfoil that results in an exit deviation angle that is optimized to minimize downstream shock induced flowfield disturbances. Specifically, a design process of a transonic airfoil minimizes pitchwise variation in downstream static pressure that includes determining an airfoil exit deviation angle and downstream turning for reduced shock from a trailing edge of the transonic airfoil.
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title	Process to minimize turbine airfoil downstream shock induced flowfield disturbance
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