Effect of Film Cooling on Entropy Noise Generation in a Stator Blade Row-Reference-Cited by-同舟云学术

Effect of Film Cooling on Entropy Noise Generation in a Stator Blade Row

Published:2021-05-10 Issue: Volume: Page:1-16
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Bach Thomas¹,Huet Maxime²,Watson Rob¹,Spence Stephen¹,Mahmoudi Yasser¹

Affiliation:

1. Queen’s University Belfast, Belfast, Northern Ireland BT9 5AH, United Kingdom

2. University of Paris-Saclay, F-92322 Châtillon, France

Funder

Engineering and Physical Sciences Research Council

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference34 articles.

1. SchererC. “Global Market Forecast Cities, Airports & Aircraft 2019–2038,” AIRBUS S.A.S. 31707 Blagnac Cedex, France, 2019, https://www.airbus.com/aircraft/market/global-market-forecast.html.

2. Combustion noise

3. Acoustic disturbance from gas non-uniformities convected through a nozzle

4. The interaction of entropy fluctuations with turbine blade rows; a mechanism of turbojet engine noise

Cited by 5 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. Modeling of indirect combustion noise through a stator;Journal of Sound and Vibration;2022-12

2. An active direction control method in rotating detonation combustor;International Journal of Hydrogen Energy;2022-06

3. Effects of supersonic nozzle guide vanes on the performance and flow structures of a rotating detonation combustor;Acta Astronautica;2022-04

4. Computational Analysis of Rotating Detonation Engine Exhaust Interacting with a Turbine Vane;AIAA SCITECH 2022 Forum;2022-01-03

5. A comparative analysis of the evolution of compositional and entropy waves in turbulent channel flows;Physics of Fluids;2022-01