Airfoil–Vortex Interaction Noise Control Mechanism Based on Active Flap Control-Reference-Cited by-同舟云学术

Airfoil–Vortex Interaction Noise Control Mechanism Based on Active Flap Control

Published:2022-01 Issue:1 Volume:35 Page:04021111
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Hu Zhiyuan¹^ORCID,Xu Guohua²,Shi Yongjie³,Xia Runze¹^ORCID

Affiliation:

1. Ph.D. Candidate, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China. ORCID: .

2. Professor, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China (corresponding author).

3. Professor, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, People’s Republic of China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001356

Reference37 articles.

1. Aoyama T. C. Yang N. Kondo and S. Saito. 2006. “Comparison of noise reduction effect between AFC and conventional IBC by moving overlapped grid method.” In Proc. 12th AIAA/CEAS Aeroacoustics Conf. (27th AIAA Aeroacoustics Conf.). Fairfax VA: American Helicopter Society International.

2. Aoyama T. C. Yang and S. Saito. 2005. “Numerical analysis of active flap for noise reduction using moving overlapped grid method.” In Proc. American Helicopter Society 61st Forum. Reston VA: American Institute of Aeronautics and Astronautics.

3. Baeder J. J. Gallman and Y. Yu. 1993. “A computational study of the aeroacoustics of rotors in hover.” In Proc. 15th Aeroacoustics Conf. Reston VA: American Institute of Aeronautics and Astronautics.

4. Boxwell D. A. and F. H. Schmitz. 1980. “Full-scale measurements of blade-vortex interaction noise.” In Proc. 36th Annual National Forum of the American Helicopter Society. Fairfax VA: American Helicopter Society International.

5. Numerical Algorithms for Acoustic Integrals with Examples for Rotor Noise Prediction

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