Impact of Bypass Duct Bifurcations on Fan Noise-Reference-Cited by-同舟云学术

Impact of Bypass Duct Bifurcations on Fan Noise

Published:2014-01 Issue:1 Volume:30 Page:143-152
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Holewa Axel¹,Weckmüller Christian¹,Guérin Sébastien¹

Affiliation:

1. Engine Acoustics, Institute of Propulsion Technology, DLR, German Aerospace Center, 10623 Berlin, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34957

Reference20 articles.

1. Sound Generation in Subsonic Turbomachinery

2. HolewaA.KrögerG.NickeE.ClemenC.HerzogS. “Optimization of the Struts in a Bypass Duct of a Civil Aircraft Engine to Minimize the Circumferential Pressure Variation,” ISABE Paper ISABE-2009-1152, 2009.

3. WeckmüllerC.GuérinS.AshcroftG. “CFD/CAA Coupling Applied to DLR UHBR-Fan: Comparison to Experimantal Data,” AIAA Paper 2009-3342, 2009.

4. AshcroftG.FreyC.HeitkampK.WeckmüllerC. “Advanced Numerical Methods for the Prediction of Tonal Noise in Turbomachinery, Part 1: Implicit Runge–Kutta Schemes,” ASME Paper GT2012-69447, 2012.

5. Toward Excellence in Turbomachinery Computational Fluid Dynamics: A Hybrid Structured-Unstructured Reynolds-Averaged Navier-Stokes Solver

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