Numerical Simulations for Transport Aircraft High-Lift Configurations Using Adaptive Cartesian Grid Methods-Reference-Cited by-同舟云学术

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Numerical Simulations for Transport Aircraft High-Lift Configurations Using Adaptive Cartesian Grid Methods

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Sang Wei¹,Li Feng¹

Affiliation:

1. Northwestern Polytechnical University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4965

Reference15 articles.

1. John,C.V. "AnUnstructured-MeshEulerMethod forMultielementAirfoilGeometries",AIAAPaper90-3051 -CP,1990.

2. ShahyarPirzadh,"UnstructuredViscous Grid GenerationbyAdvancing-LayersMethod,"AIAAPaper 93-3453 -CP,1993.

3. Anderson, W. K., Bonhaus, D. L. "Numerical Study To Assess Sulfur Hexafluoride as a Medium for Testing MultielementAirfoils",NASATechnicalPaper3496,June1995.

4. Lindblad, I. A. A., de Cock, K. M. J. "Computational Fluid Dynamics Prediction of Maximum Lift of a Two-DimensionalHighLiftConfiguration,"AIAAPaper99-3180,1999.

5. Rogers,S.E."ProgressinHigh-liftAerodynamicsCalculations,"AIAAPaper93-0194,1993.

Cited by 1 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. Icing Effect Study for Wing/Body and High-Lift Wing Configurations;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

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