Aeroacoustics of NACA 0018 Airfoil with a Cavity-Reference-Cited by-同舟云学术

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Aeroacoustics of NACA 0018 Airfoil with a Cavity

Published:2018-12 Issue:12 Volume:56 Page:4775-4786
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Lam Garret C. Y.¹,Leung Randolph C. K.¹

Affiliation:

1. The Hong Kong Polytechnic University, Hong Kong, People’s Republic of China

Funder

Philip K. H. Wong Foundation

Hong Kong Polytechnic University

State Key Laboratory of Mechanical System and Vibration, Shanghai Jiao Tong University

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056389

Reference30 articles.

1. AERODYNAMICS OF SMALL VEHICLES

2. Parametric study of separation and transition characteristics over an airfoil at low Reynolds numbers

3. Trapped vortices and a favourable pressure gradient

4. Inviscid Batchelor-model flow past an airfoil with a vortex trapped in a cavity

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