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NASA NTRS ยท 20050214035

Compressor Flow Control Concepts: UEET Compressor Flow Control Modeling - 2

Abstract

Several passive flow control devices have been modeled computationally in the Swift CFD code. The models were applied to the first stage rotor and stator of the baseline UEET compressor in an attempt to improve efficiency and/or stall margin. The devices included suction surface bleed, tip injection, self-aspirated rotors, area-ruled casing, and vortex generators. The models and computed results will be described in the presentation. None of the results have shown significant gains in efficiency; however, casing vortex generators have shown potential improvements in stall margin.

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BibTeXRIS

Chima, Rodrick V.. 2001-01-01. Compressor Flow Control Concepts: UEET Compressor Flow Control Modeling - 2. https://ntrs.nasa.gov/citations/20050214035

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