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Effect of Cascade Parameters on Rotating Stall (1959)

Seidel, B. S. ; Senoo, Y. ; Stenning, A. H.

In: CASI

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Publication Date: 2019-08-17

Description: Analysis of the vortex model proposed by Kriebel, Seidel, and Schwind shows this representation of rotating stall satisfies, at least approximately, the requirements at the cascade. Cascade-parameter-variation effects on rotating stall were studied in a circular cascade and single-stage compressor. Modification of the single-stage compressor stopped the rotating-stall pattern and permitted observation of the pressure and velocity distribution around the annulus. Closer observation might be possible with proper flow-visualization techniques, such as a water pump.

Keywords: Aircraft Design, Testing and Performance

Type: NASA-MEMO-3-16-59W

Format: application/pdf

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