Effects of pre-swirl radius on cooling performance of a rotor-stator pre-swirl system in gas turbine engines-Reference-Cited by-同舟云学术

Effects of pre-swirl radius on cooling performance of a rotor-stator pre-swirl system in gas turbine engines

Published:2022-09 Issue: Volume:37 Page:102250
ISSN:2214-157X
Container-title:Case Studies in Thermal Engineering
language:en
Short-container-title:Case Studies in Thermal Engineering

Author:

Kong Xiaozhi^ORCID,Huang Tianshuo,Liu Yuxin,Chen Hua,Lu Huawei

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Engineering (miscellaneous)

Reference33 articles.

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2. An Investigation of a Preswirled Cooling Airflow to a Turbine Disc by Measuring the Air Temperature in the Rotating Channels. ASME Paper No. 81-GT-132;Meierhofer,1981

3. Pre-swirl blade-cooling effectiveness in an adiabatic rotor-stator system;El-Oun;ASME J. Turbomach.,1989

4. High pressure turbine low radius radial TOBI discharge coefficient validation process;Mirzamoghadam;J. Fluid Eng.,2013

5. Discharge coefficients of a preswirl system in secondary air systems;Dittmann;ASME J. Turbomach.,2002

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