The influence of blade wakes on the performance of combustor shortened prediffusers

Author:

Stevens S. J.1,Harasgama S. P.1,Wray P.2

Affiliation:

1. University of Technology, Loughborough, England

2. Rolls-Royce Ltd., Derby, England

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 19 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Effect of Compressor Unsteady Wakes on a Gas Turbine Combustor Flow;Journal of Engineering for Gas Turbines and Power;2022-10-14

2. Aerothermal Technologies for Low Emissions Combustors;Sustainable Development for Energy, Power, and Propulsion;2020-09-04

3. Experimental study of the effect of impeller blades different shape on centrifugal pump performance;IOP Conference Series: Materials Science and Engineering;2020-02-01

4. Influence of Purge Flow Swirl at Exit to the High-Pressure Compressor on OGV/Pre-Diffuser and Combustion System Aerodynamics;Journal of Turbomachinery;2019-06-14

5. Impact of a Cooled Cooling Air System on the External Aerodynamics of a Gas Turbine Combustion System;Journal of Engineering for Gas Turbines and Power;2017-01-10

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