NASA Trapezoidal-Wing Simulation Using Stress-ω, and One- and Two-Equation Turbulence Models-Reference-Cited by-同舟云学术

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NASA Trapezoidal-Wing Simulation Using Stress-ω, and One- and Two-Equation Turbulence Models

Published:2015-07 Issue:4 Volume:52 Page:1189-1200
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Rodio J. J.¹,Xiao X.²,Hassan H. A.¹,Rumsey C. L.³

Affiliation:

1. Mechanical and Aerospace Engineering, North Carolina State University, Raleigh, North Carolina 27695-7910

2. Corvid Technologies, Mooresville, North Carolina 28117-8006

3. Computational AeroSciences Branch, NASA Langley Research Center, Hampton, Virginia 23681-2100

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032848

Reference25 articles.

1. WilcoxD. C., Turbulence Modeling for CFD, 3rd ed., DCW Industries, La Cañada, CA, 2006, pp. 332–333.

2. KristS. L.BiedronR. T.RumseyC. L. “CFL3D User’s Manual (Ver. 5.0),” NASA TM-1998-208444, June 1998.

3. Two-equation eddy-viscosity turbulence models for engineering applications

4. Summary of the First AIAA CFD High-Lift Prediction Workshop

Cited by 2 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. Aerodynamic optimization of high-lift devices using a 2D-to-3D optimization method based on deep reinforcement learning and transfer learning;Aerospace Science and Technology;2022-02

2. Application of a Full Reynolds Stress Model to High Lift Flows;46th AIAA Fluid Dynamics Conference;2016-06-10

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