Practical Large-Eddy Simulation for Complex Turbulent Flowfield with Adaptive Cartesian Mesh and Data Compression Technique
Author:
Affiliation:
1. Tohoku University
2. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2862
Reference26 articles.
1. 1Nakahashi,K."High-DensityMesh FlowComputationswith Pre-/Post-DataCompressions,"AIAAPaper2005-4876,2005.
2. 3Takahashi,S.,Ishida,T.,Nakahashi,K.,Kobayashi,H.,Okabe,K., Shimomura,Y.,Soga,T.,andMusa, A."StudyofHigh Resolution IncompressibleFlow Simulation Basedon Cartesian Mesh,"AIAAPaper 2009-0563,2009.
3. 4Onda, H., Sakai, R., Sasaki, D., Nakahashi, K. "Unsteady Flow and Aerodynamic Noise Analysis around JAXA Landing GearModelbyBuilding-CubeMethod," AIAAPaper2011-1081,2011.
4. 5Deguchi,A., Sasaki,D., Nakahashi,K.,Murayama,M.,Yamamoto, K., andYokokawa,Y. "Aeroacoustic Simulation of JAXA Landing Gear byBuilding-CubeMethod andNon-compact Curle's Equation,"AIAAPaper2012-0388,2012.
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