The effect of variations in first- and second-order derivatives on airfoil aerodynamic performance-Reference-Cited by-同舟云学术

The effect of variations in first- and second-order derivatives on airfoil aerodynamic performance

Published:2016-12-04 Issue:1 Volume:11 Page:54-68
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Yi Penghui¹²,Wang Ying¹²,Sun Xiaojing¹²,Huang Diangui¹²,Zheng Zhongquan³

Affiliation:

1. School of Energy and Power Engineering, University of Shanghai for Science and Technology, Shanghai, China

2. Shanghai Key Laboratory of Multiphase Flow and Heat Transfer of Power Engineering, University of Shanghai for Science and Technology, Shanghai, China

3. Aerospace Engineering Department, University of Kansas, Lawrence, Kansas, USA

Publisher

Informa UK Limited

Subject

Modeling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2016.1246264

Reference20 articles.

1. Gregory, N. & OReilly, C. (1970). Low-speed aerodynamic characteristics of NACA 0012 aerofoil section including the effects of upper-surface roughness simulating hoar frost. NASA R&M 3726.

2. Unified computation of flow with compressible and incompressible fluid based on roe’s scheme

3. A computational method for cavitational flows based on energy conservation

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