GPU-Accelerated Implicit Large Eddy Simulation of a NACA 0018 Airfoil with Active Flow Control-Reference-Cited by-同舟云学术

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GPU-Accelerated Implicit Large Eddy Simulation of a NACA 0018 Airfoil with Active Flow Control

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
language:
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Author:

Laufer Michael¹,Frankel Steven H.¹,Greenblatt David¹

Affiliation:

1. Technion Israel Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0471

Reference24 articles.

1. Mechanisms for laminar separated-flow control using dielectric-barrier-discharge plasma actuator at low Reynolds number

2. Airfoil in a high amplitude oscillating stream

3. Computations of Active Flow Control Via Steady Blowing Over a NACA-0018 Airfoil: Implicit LES and RANS Validated Against Experimental Data

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. Effects of Boundary Layer Suction on a Laminar Separation Bubble on a HLFC Wing;AIAA AVIATION 2023 Forum;2023-06-08

2. GPU-Accelerated Numerical Study of Temperature Effects in Choked Under-expanded Supersonic Jets;AIAA SCITECH 2023 Forum;2023-01-19

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