Rod–Airfoil Interaction Noise at Different Rod Cross Sections and Airfoil Angles
Author:
Affiliation:
1. Wenzhou University, 325035 Wenzhou, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061303
Reference45 articles.
1. Prediction of Rod-Airfoil Interaction Noise Using the Ffowcs-Williams-Hawkings Analogy
2. A rod-airfoil experiment as a benchmark for broadband noise modeling
3. MagagnatoF.SorgűvenE.GabiM. “Far-Field Noise Prediction by Large-Eddy Simulation and Ffowcs-Williams and Hawkings Analogy,” AIAA Paper 2003-3206, July 2003.
4. Wake-Airfoil Interaction as Broadband Noise Source: A Large-Eddy Simulation Study
5. BerlandJ.LafonP.CrouzetF.DaudeF.BaillyC. “Numerical Insight into Sound Sources of a Rod-Airfoil Flow Configuration Using Direct Noise Calculation,” AIAA Paper 2010-3705, July 2010.
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