Experimental Investigation of the Flow Characteristics and Noise Generation at the Wing

Experimental Investigation of the Flow Characteristics and Noise Generation at the Wing–Wall Junction

Published:2021-09 Issue:5 Volume:34 Page:04021054
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Ding Y.¹^ORCID,Zhang T.²,Geyer T. F.³,de Silva C. M.⁴,Doolan C. J.⁵^ORCID,Moreau D. J.⁶^ORCID

Affiliation:

1. Ph.D. Student, School of Mechanical and Manufacturing Engineering, Univ. of New South Wales, Sydney 2052, Australia (corresponding author). ORCID: .

2. Ph.D. Student, School of Mechanical and Manufacturing Engineering, Univ. of New South Wales, Sydney 2052, Australia.

3. Lecturer, Technical Acoustics Group, Brandenburg Univ. of Technology Cottbus–Senftenberg, Cottbus 03046, Germany.

4. Lecturer, School of Mechanical and Manufacturing Engineering, Univ. of New South Wales, Sydney 2052, Australia.

5. Professor, School of Mechanical and Manufacturing Engineering, Univ. of New South Wales, Sydney 2052, Australia. ORCID: .

6. Senior Lecturer, School of Mechanical and Manufacturing Engineering, Univ. of New South Wales, Sydney 2052, Australia. ORCID: .

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.1943-5525.0001303

Reference31 articles.

1. Abdulla-Altaii A. K. and R. R. Raj. 1994. “Three-dimensional flow structure in the wake of a wing-body juncture.” In Proc. AIAA Fluid Dynamics Conf. 1994. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.1994-2289.

2. Flow structure of a low aspect ratio wall-mounted airfoil operating in a low Reynolds number flow

3. The Effect of Aspect Ratio on Wall Pressure Fluctuations at a Wing-Plate Junction

4. A Survey of Time-Averaged Characteristics of Laminar and Turbulent Horseshoe Vortices

Cited by 1 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. Wing Tip Vortex Formation Noise;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13