Discrete tones in subsonic jet engine test cells-Reference-Cited by-同舟云学术

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Discrete tones in subsonic jet engine test cells

Published:2018-08 Issue: Volume:101 Page:49-60
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:en
Short-container-title:Progress in Aerospace Sciences

Author:

Desmarais G.,Rocha J.

Funder

Consortium of Aerospace Research in Canada

Natural Sciences and Engineering Research Council of Canada

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference71 articles.

1. Scale model testing of infrasound produced by various jet engine test cell configurations;Hatlestad,2006

2. Jet Engine Test Cell Noise Reduction;Kodres,2000

3. Investigation into the Vortex Formation Threshold and Infrasound Generation in a Jet Engine Test Cell;Wei Hua,2009

4. The acoustic response of altitude test facility exhaust systems to axisymmetric and two-dimensional turbine engine exhaust plumes;Jones,1992

5. Self-excited oscillations in jet engine test cells;Howe;J. Fluid Struct.,1986

Cited by 2 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. Identification of Discrete Tonal Noise in Inclined Jet Impingement Using Pressure-Sensitive Paint;AIAA Journal;2023-02

2. Turbulent kinetic energy and self-sustaining tones: Experimental study of a rectangular impinging jet using high Speed 3D tomographic Particle Image Velocimetry;Journal of Mechanical Engineering and Sciences;2020-03-23

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