Effect of Rotor Shielding on Fan-Outlet Guide Vanes Broadband Noise Prediction-Reference-Cited by-同舟云学术

Effect of Rotor Shielding on Fan-Outlet Guide Vanes Broadband Noise Prediction

Published:2013-07 Issue:7 Volume:51 Page:1576-1592
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Posson Hélène¹,Moreau Stéphane²

Affiliation:

1. Centre for Mathematical Sciences, University of Cambridge, Cambridge, England CB3 0WA, United Kingdom

2. Mechanical Engineering Department, Université de Sherbrooke, Sherbrooke, Quebec J1K 2R1, Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J051784

Reference61 articles.

1. A reflection mechanism for aft fan tone noise from turbofan engines

2. Mode trapping in coupled 2D cascades - Aerodynamic and acoustic results

3. HansonD. B. “Coupled 2-Dimensional Cascade Theory for Noise and Unsteady Aerodynamics of Blade Row Interaction in Turbofans. Vol. 1: Theory Development and Parametric Studies,” NASA CR-4506, 1994.

4. TopolD. A. “TFaNS Tone Fan Noise Design/Prediction System. Vol. 3: Evaluation of System Codes,” NASA CR-1999-208884, 1999.

5. TopolD. A. “TFaNS Tone Fan Noise Design/Prediction System. Vol. 1: System Description, CUP3D Technical Documentation and Manual for Code Developers,” NASA CR-1999-208882, 1999.

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