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NASA NTRS ยท 19930050314

Turbulence and stall in plane diffusers - Computational study

Abstract

The effect of free-stream turbulence level on stall conditions in plane diffusers is investigated with a finite-volume numerical method which utilizes a k-epsilon turbulence model or a differential Reynolds stress model for closure. Computed results show qualitative agreement with measured data. The ability to eliminate stall and thereby increase pressure recovery in diffusers at large included angles by utilizing high free-stream turbulence is correctly predicted.

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BibTeXRIS

Demuren, A. O.. 1991-01-01. Turbulence and stall in plane diffusers - Computational study. https://ntrs.nasa.gov/citations/19930050314

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