Validation of Flows on High-Lift Configurations by Structured and Unstructured Mesh Method-Reference-Cited by-同舟云学术

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Validation of Flows on High-Lift Configurations by Structured and Unstructured Mesh Method

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Murayama Mitsuhiro¹,Yamamoto Kazuomi¹,Kobayashi Kunihiko²

Affiliation:

1. Japan Aerospace Exploration Agency

2. Ryoyu Systems Co., Ltd.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1226

Reference29 articles.

1. Flap-Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport Wing

2. Prediction of high lift: review of present CFD capability

Cited by 12 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. Study of Civil-Plane High-Lift Model Using Omni-Tree Cartesian Grids;Applied Mechanics and Materials;2012-12

2. Unstructured Adaptive Mesh Calculations for NASA Trap Wing Using the Code HiFUN;30th AIAA Applied Aerodynamics Conference;2012-06-25

3. Noise Simulation around NACA0012 Wingtip using Large Eddy Simulation;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2012

4. Numerically analyzing more efficiently high-lift aerodynamics of wing/body model with omni-tree Cartesian grids;Aerospace Science and Technology;2011-07

5. Robust Cartesian Grid Flow Solver for High-Reynolds-Number Turbulent Flow Simulations;AIAA Journal;2010-06

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