Numerical simulation of aircraft wake vortex evolution and wake encounters based on adaptive mesh method-Reference-Cited by-同舟云学术

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Numerical simulation of aircraft wake vortex evolution and wake encounters based on adaptive mesh method

Published:2020-01-01 Issue:1 Volume:14 Page:1445-1457
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Zhou Jinxin¹,Chen Yingchun¹²,Li Dong¹,Zhang Zeyu¹,Pan Weijun³

Affiliation:

1. School of Aeronautics, Northwestern Polytechnical University, Xi’an, People’s Republic of China

2. Commercial Aircraft Corporation of China, Ltd., Shanghai, China

3. College of Air Traffic Management, Civil Aviation Flight University of China, Guanghan, People’s Republic of China

Funder

National Natural Science Foundation of China

Publisher

Informa UK Limited

Subject

Modeling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2020.1835736

Reference32 articles.

1. Experimental and computational fluid dynamics-based numerical simulation of using natural gas in a dual-fueled diesel engine

2. Towards the Applicability of the Modified von Kármán Spectrum to Predict Trailing Edge Noise

3. Stochastic approach to noise modeling for free turbulent flows

4. Simulation Methods for Aircraft Encounters with Deformed Wake Vortices

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