Measurements of fan inflow distortion noise generation in a low speed fan - part I: aerodynamic analyses-Reference-Cited by-同舟云学术

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Measurements of fan inflow distortion noise generation in a low speed fan - part I: aerodynamic analyses

Published:2022-06-13 Issue: Volume: Page:
ISSN:
Container-title:28th AIAA/CEAS Aeroacoustics 2022 Conference
language:
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Author:

Caldas Luciano¹,Klähn Lukas¹,Meyer Robert¹,Tapken Ulf¹

Affiliation:

1. Deutsches Zentrum fur Luft- und Raumfahrt eV

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2944

Reference25 articles.

1. Cousins, W. T. “History, philosophy, physics, and future directions of aircraft propulsion system/inlet integration,” Turbo Expo: PowerforLand,Sea,andAir.Vol.41677,2004.

2. Kantola, R. A., and Warren, R. E. “Basic research in fan source noise: Inlet distortion and turbulence noise,” Tech. rep., NASA-CR-159451,1978.

3. Conrad,M.P.H.,E.William,andMcAulay,J.E.“EffectsofInlet-Air-FlowDistortiononSteady-StateAltitudePerformanceof anAxial-FlowTurbojetEngine,”Tech.rep.,NATIONALAERONAUTICSANDSPACEADMINISTRATIONWASHINGTON DC,1955.

Cited by 1 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. Inflow Distortion Noise and Turbulence Measurements in a Low Speed Fan Test Rig;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

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