(Journal of the Japan Society for Aeronautical and Space Sciences), 54 (625), 82-88, 2006. (Design Exploration of Aerodynamic Wing Shape for RLV Flyback Booster)” Vol.54, No.627, pp.144-150, 2006 Togashi, F., Ito, Y., Nakahashi, K. and Obayashi, S., “Overset Unstructured Grids Method for Viscous Flow Computations,” AIAA Journal, Vol.44, No.7, pp.1617-1623, July, 2006 , (Aerodynamic Analyses of Airfoil Configuration of Biplane Type Supersonic Transport),” Vol.71, No.721 B , pp.50-57, Sept. 2006. Salim Koc, Hyoung-Jin Kim and Kazuhiro Nakahashi, “Aerodynamic Design of Complex Configurations with Junctions,” Journal of Aircraft 2006, Vol.43 No.6, pp.1838-1844, Nov.-Dec.2006. H.-J. Kim, Y. Takano and K. Nakahashi, “Error Estimation and Grid Adaptation Using Euler Adjoint Method,” Journal of Aircraft, Vol. 43, No. 5, Nov.-Dec.2006 Yasushi Ito, Alan M. Shih, Bharat K. Soni and Kazuhiro Nakahashi, “Multiple Marching Direction Approach to Generate High Quality Hybrid Meshes,” AIAA Journal, vol.45 No.1, pp.162-167, Jan. 2007. Chiba, K., Oyama, A., Obayashi, S., Nakahashi, K., Morino, H., “Multidisciplinary Design Optimization and Data Mining for Transonic Regional-Jet Wing,” J. Aircraft, Vol.44, No. 4, pp.1100-1112, 2007. Kazuhisa Chiba, Shigeru Obayashi and Kazuhiro Nakahashi, “Open-Type Separation on Delta Wings for Leading-Edge Bluntness”, Trans. Japan Soc. Aero. Space Sci., 50(168), 81-87, Aug., 2007 Ito, Y., Shih, A. M., Erukala, A. K., Soni, B. K., Chernikov, A. N., Chrisochoides, N. P. and Nakahashi, K., "Parallel Mesh Generation Using an Advancing Front Method," Mathematics and Computers in Simulation, Vol. 75, Issues 5-6, September 2007, pp. 200-209. Hyoung-Jin Kim and Kazuhiro Nakahashi, “Surface Mesh Movement for Aerodynamic Design of Body-Installation Junction,” AIAA J., Vol.45, No.5, 2007. Yamazaki, W., Matsushima, K., Nakahashi, K., "Drag Prediction, Decomposition and Visualization in Unstructured Mesh CFD Solver of TAS-code", International Journal for Numerical Methods in Fluids, accepted for publication. Yamazaki, W., Matsushima, K., Nakahashi, K., “Drag Decomposition-Based Adaprive Mash -26-
efinement”, journal of Aircraft, accepted for publication. K. Nakahashi, “Flow around a Bee, Unstructured Grid Generation,”Invited lecture at the 5th Asian Computational Fluid Dynamics, Busan, Korea, Oct. 2003. K. Nakahashi, “Vision of Asian Passenger Plane for the 21th Century”, Key Note Lecture at the Asian Passenger Plane Forum 2003, Taipei, Oct. 2003. K. Nakahashi and L-S. Kim, “Building-Cube Method for Large-Scale, High Resolution Flow Computations”, AIAA 2004-0434, 42nd AIAA Aerospace Science Meeting and Exhibit, Reno, NV, January 2004. K. Nakahashi and L-S. Kim, “Building-Cube Method for Large-Scale, High Resolution Flow Computations”, AIAA 2004-0434, 42nd AIAA Aerospace Science Meeting and Exhibit, Reno, NV, January 2004. K. Nakahashi, and L-S. KIM, “High-Density Mesh Flow Computations by Building-Cube Method”, International Conference of CFD (ICCFD), Toronto, July 2004. K. Nakahashi and L-S. Kim, “High-Density Mesh Computations of Airfoil Flows by Building-Cube Method”, Parallel Computational Fluid Dynamics 2004, Gran Canaria, Canary Islands, Spain. May 24-27, 2004 H. J. Kim, Y. Takano and K. Nakahashi, “Error Estimation and Grid Adaptation Using Euler Adjoint Method,” AIAA-2005-5336, AIAA CFD Conference, Toronto, Canada, June, 2005. H. J. Kim, Y. Takano and K. Nakahashi, “Adjoint-Based Adaptive Mesh Refinement for Three Dimensional Euler Analysis,” 2005 JSASS-KSAS Joint International Symposium on Aerospace Engineering, Nagoya, JAPAN, October, 2005. Kazuhiro Nakahashi, Aya Kitoh, Yuta Sakurai, “Three- Dimensional Flow Computations Around an Airfoil by Building- Cube Method”, AIAA Paper 2006-1104, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2006. Hyoung-Jin Kim, Kazuhiro Nakahashi,“Output- Based Error Estimation and Adaptive Mesh Refinement Using Viscous Adjoint Method”, AIAA-2006-1395, 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2006. -27-
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