Automatic Grid Generation of Complete Aircraft Model in Wind Tunnel Test for Navier-Stokes Simulation-Reference-Cited by-同舟云学术

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Automatic Grid Generation of Complete Aircraft Model in Wind Tunnel Test for Navier-Stokes Simulation

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Lahur Paulus¹,Hashimoto Atsushi²,Murakami Keiichi²

Affiliation:

1. Research Center of Computational Mechanics, Inc.

2. Japan Aerospace Exploration Agency (JAXA)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-555

Reference14 articles.

1. 1Lahur,P.R."AutomaticHexahedraGrid Generation MethodforComponent-based Surface Geometry,"AIAApaper 2005-5242,2005.

2. 2Hashimoto, A., Murakami, K., Aoyama, T., Lahur P. "Lift and Drag Prediction Using Automatic Hexahedra Grid Generation Method,"AIAApaper 2009-1365.

3. 3Hashimoto, A., etal, "Drag Prediction on NASA CRM using Automatic Hexahedra Grid Generation," AIAA Paper 2010-1417,2010.

4. 5Deister, F. and Hirschel, E.H. "Adaptive Cartesian/Prism Grid Generation and Solutions for Arbitrary Geometries," AIAA paper 99-0782,1999.

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