Tohoku Univ. Institute of Fluid Science

Obayashi Jeong Laboratory

• English Top
• Prof. Obayashi
• Staff
• Students
• Laboratory
• Research Topics
• Publications
• Events
• Schedule
• Links
• Japanese Page

Publications

In this page, latest papers are introduced. You can download part of them by PDF.

Last update: 8/31/07

• GECCO-99 - one-page paper for poster session
• CFD 99 - Canada
• AIAA CFD 99 - Norfolk, VA
• SMC 99 - Tokyo
• ICNPAA 00 - Dytna Beach
• 1st ICCFD - unstructured adjoint method - Kyoto
• ECCOMAS 2K - Barcelona
• PPSN VI - Paris
• International Session in Aircraft Symposium - Flutter simulation - Sendai
• EMO'01 - Zurich, Switzerland
• CFD2001 - Waterloo, Canada
• AIAA CFD 01 - Anaheim, CA
  
• AIAA Paper 2002-0836 - Nacelle integration
• AIAA Paper 2002-0991 - SOM
• AIAA Paper 2002-5549 - SST wing-body optimization
• ICAS2002 - Aileron buzz
• PPSN VII - MOGA for Car Engine
• EMO2003 - Faro, Portugal
• Shigeru Obayashi and Daisuke Sasaki, Visualization and Data Mining of Pareto Solutions Using Self-Organizing Map, Second International Conference on Evolutionary Multi-Criterion Optimization, Faro, Portugal, LNCS 2632, Springer-Verlag Berlin Heidelberg 2003, pp. 796-809, April 2003.
• AIAA CFD 03 - Orlando, FL
• Finding Tradeoffs by Using Multiobjective Optimization Algorithms
• Shigeru OBAYASHI, Daisuke SASAKI and Akira OYAMA, "Finding Tradeoffs by Using Multiobjective Optimization Algorithms", Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 47, No. 155, pp. 51-58, MAY 2004.
• Color figures for the chapter in Applications of Multi-Objective Evolutionary Algorithms (4.8MB) 2004
• Shigeru Obayashi and Daisuke Sasaki, "Multiobjective Aerodynamic Design and Visualization of Supersonic Wings by Using Adaptive Range Multiobjective Genetic Algorithms (chapter 13)," Coello Coello and Lamont (eds.), Applications of Multi-Objective Evolutionary Algorithms, World Scientific Publishing, New Jersey, 2004.
• EMO2005 - Guanajuato, Mexico (Link to Springer web site)
• Chiba, K., Obayashi, S., Nakahashi, K., and Morino, H., "High-Fidelity Multidisciplinary Design Optimization of Wing Shape for Regional Jet Aircraft," Third International Conference on Evolutionary Multi-Criterion Optimization, Guanajuato, Mexico, LNCS 3410, Springer-Verlag Berlin Heidelberg 2005, pp. 621-635, March 2005.
• AIAA Paper 2005-4604 - Supersonic formation flight
• Y. Goto, S.Obayashi and Y. Kohama, "Drag Characteristics of a Low-Drag Low-Boom Supersonic Formation Flying Concept," AIAA Paper 2005-4604, 35th AIAA Fluid Dynamics Conference and Exhibit, 6-9 June 2005, Toronto Canada.
• AIAA Paper 2005-4666 - Multi-Objective Design Exploration (MODE) revision in references 8/22/07
• Shigeru Obayashi, Shinkyu Jeong and Kazuhisa Chiba, "Multi-Objective Design Exploration for Aerodynamic Configurations," AIAA Paper 2005-4666 (invited), 35th AIAA Fluid Dynamics Conference and Exhibit, 6-9 June 2005, Toronto Canada.
• AIAA Paper 2005-5079 - Data Mining
• Jeong, S., Chiba, K., and Obayashi, S., "Data Mining for Aerodynamic Design Space," AIAA Paper 2005-5079, AIAA 23rd Applied Aerodynamics Conference, Toronto, Canada, June 2005.
• AIAA Paper 2005-5080 - MDO for Regional Jet
• Chiba, K., Obayashi, S., Nakahashi, K., and Morino, H., "High-Fidelity Multidisciplinary Design Optimization of Aerostructural Wing Shape for Regional Jet," AIAA Paper 2005-5080, AIAA 23rd Applied Aerodynamics Conference, Toronto, Canada, June 2005.
• ECCOMAS-2006 - Edmond aan Zee NEW
• Shigeru Obayashi, "Multi-objective design exploration using efficient global optimization," European Conference　on Computational Fluid Dynamics，Edmond aan Zee，The Netherlands, 2006 Sep.

MISORA related links: Yamashita, Yonezawa

List of paper (journals and books)

1. Jeong, S., Matsushima, K., Iwamiya, T., Obayashi, S. and Nakahashi, K., “Inverse Design of Supersonic Airfoils Using Integral Equations,” Journal of Aircraft, Vol. 36, No. 3, pp. 606-608, May-June 1999.
2. Obayashi, S. and Takeguchi, Y., "Multipoint Aerodynamic Design of Supersonic Wing Planform Using MOGA," Proceedings of the Seventh Annual Conference of the Computational Fluid Dynamics Society of Canada, Halifax,  June, 1999.
3. Oyama, A., Obayashi, S., Nakahashi, K. and Hirose, N., "Fractional Factorial Design of Genetic Coding for Aerodynamic Optimization," AIAA Paper 99-3298, June 1999.
4. Oyama, A., Obayashi, S and Nakahashi, K., "Wing Design Using Real-Coded Adaptive Range Genetic Algorithm," to be published in Proceedings of 1999 IEEE International Conference on Systems, Man, and Cybernetics, Tokyo, October 12-15, 1999.
5. Oyama, A., Obayashi, S., Nakahashi, K. and Nakamura, T., “Euler/Navier-Stokes Optimization of Supersonic Wing Design Based on Evolutionary Algorithm,” AIAA Journal, Vol. 37, No. 10, pp. 1327-1329, October 1999.
6.  Takahashi, S., Obayashi, S. and Nakahashi, K., "Inverse Design Optimization of Transonic Wings Based on Multi-objective Genetic Algorithms," AIAA Journal, Vol. 37, No. 12, pp. 1656-1662, December 1999.
7. Oyama, A., Obayashi, S., Nakahashi, K., and Hirose, N., "Aerodynamic Wing Optimization via Evolutionary Algorithms Based on Structured Coding," CFD Journal, Vol. 8, No. 1, pp. 570-577, January 2000.
8. Oyama., A., Obayashi, S., and Nakahashi, K., "Real-Coded Adaptive Range Genetic Algorithm and Its Application to Aerodynamic Design," JSME International Journal, Series A, Vol. 43, No. 2, pp. 124-129, February 2000.
9. Obayashi, S., Tsukahara, T., and Nakamura, T., "Multiobjective Genetic Algorithm Applied to Aerodynamic Design of Cascade Airfoils," IEEE Transactions on Industrial Electronics, Col. 47, No. 1, pp. 211-216, February 2000.
10. Oyama, A., Obayashi, S., Nakahashi, K., and Nakamura, T., "Aerodynamic Optimization of Transonic Wing Design Based on Evolutionary Algorithm," Third International Conference on Nonlinear Problems in Aviation and Aerospace Methods and Software, Daytona Beach, FL, USA, May 10-12, 2000.
11. Kim, H-J., Sasaki, D., Obayashi, S., and Nakahashi, K., "Aerodynamic Optimization of Supersonic Transport Wing Using Unstructured Adjoint Method," The First International Conference on Computational Fluid Dynamics, Kyoto, Japan, July 10-14, 2000.
12. Obayashi, S., Sasaki, D., Takeguchi, Y., and Hirose N., "Multiobjective Evolutionary Computation for Supersonic Wing-Shape Optimization," IEEE Transactions on Evolutionary Computation, Vol. 4, No. 2, pp. 182-187, July 2000.
13. Pambagjo, T. E., Nakahashi, K., and Obayashi, S., "Inverse Design of a Thick Supercritical Airfoil," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 43, No. 140, pp. 61-66, August 2000.
14. Sasaki, D., Obayashi, S., Sawada, K., and Himeno, R., "Multiobjective Aerodynamic Optimization of Supersonic Wings Using Navier-Stokes Equations," European Congress on Computational Methods in Applied Sciences and Engineering, Barcelona, Spain, September 11-14, 2000.
15. Obayashi, S., Oyama., A., and Nakamura, T., "Real-Coded Adaptive Range Genetic Algorithm Applied to Transonic Wing Optimization," The Sixth International Conference on Parallel Problem Solving from Nature, Paris, France, September 16-20, 2000.
16. 45. Obayashi, S., Oyama, A., and Nakamura, T., "Transonic Wing Shape Optimization Based on Evolutionary Algorithms," High Performance Computing, Valero, Joe, Kitsuregawa and Tanaka (Eds.), Third International Symposium, ISHPC 2000, Tokyo, Japan, Proceedings, Springer-Verlag, Berlin, October 2000.
17. Pambagjo, T. E., Nakahashi, K., Obayashi, S., and Matsushima, K., "Aerodynamic Design of a Medium Size Blended-Wing-Body Airplane," AIAA Paper 2001-0129, January 2001.
18. Murayama, M. E., Nakahashi, K., and Obayashi, S., "Numerical Simulation of Vortical Flows Using Vorticity Confinement Coupled with Unstructured Grid," AIAA Paper 2001-0606, January 2001.
19. Sasaki, D., Morikawa, M., Obayashi, S., and Nakahashi, K., "Aerodynamic Shape Optimization of Supersonic Wings by Adaptive Range Multiobjective Genetic Algorithms," Evolutionary Multi-Criterion Optimization, Zitzler, Deb, Thiele, Coello, Corne (Eds.), First International Conference, EMO 2001, Zurich, Switzerland, Proceedings, Lecture Notes in Computer Science (LNCS) Vol. 1993, Springer-Verlag, Berlin, March 2001.
20. Sasaki, D., Obayashi, S., and Kim, H.-J., "Evolutionary Algorithm vs. Adjoint Method Applied to SST Shape Optimization," CFD2001, The Annual Conference of CFD Society of Canada,, Waterloo, Canada, May 27 - 29, 2001. (CD-ROM)
21. Sasaki, D., Obayashi, S., and Nakahashi, K., "Navier-Stokes Optimization of Supersonic Wings with Four Design Objecives Using Evolutionary Algorithm," AIAA-2001-2531, 15th AIAA CFD Conference, Anaheim, CA, June 2001. (CD-ROM)
22. Kim, H.-J., Sasaki, D., Obayashi, S., and Nakahashi, K., "Aerodynamic Optimization of Supersonic Transport Wing Using Unstructured Adjoint Method," AIAA Journal, Vol. 39, No. 6, pp. 1011-1020, June 2001.
23. Kim, H.-J., Obayashi, S., and Nakahashi, K., "Flap-Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport Wing," Journal of Aircraft, Vol. 38, No. 4, pp. 709-717, July-August 2001.
24. Kanazaki, M., Obayashi, S., and Nakahashi, K., "DESIGN OPTIMIZATION OF EXHAUST MANIFOLD FOR A CAR ENGINE USING MOGA," presented at EUROGEN2001, Athens, September, EVOLUTIONARY METHODS FOR DESIGN, OPTIMISATION AND CONTROL, K. Giannakoglou, D. Tsahalis, J. Periaux, K. Papailiou and T. Fogarty (Eds.), c CIMNE, Barcelona 2002, in print.
    
25. Yang, G. W., Kondo, M. and Obayashi, S., "Multiblock Navier-Stokes Solver for Wing/Fuselage Transport Aircraft," Proceedings of the First International Symposium on Advanced Fluid Information, Zao, October, 2001, pp. 396-401.
26. Yang, G. W., Obayashi, S. and Nakamichi, J., "Aeroelastic Simulation on SST with Multiblock Moving Grid Algorithm," Preprint of 3rd International Workshop on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport, December 2001, proceedings in print.
27. Kondo, M. Yang, G. W., and Obayashi, S., "Multiblock Navier-Stokes Solver for SST Wing-Fuselage Configuration," Preprint of 3rd International Workshop on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport, December 2001, proceedings in print.
28. Sasaki, D. and Obayashi, S., "Automated Aerodynamic Design Optimization System for SST Wing-Body Configuration," Preprint of 3rd International Workshop on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport, December 2001, proceedings in print.
29. Kanazaki, M., Obayashi, S., and Nakahashi, K., "NUMERICAL SIMULATION OF SUPERSONIC FLOW AROUND WING-BODY CONFIGURATION WITH INTEGRATED ENGINE NACELLE," AIAA-Paper 2002-0836, Jan. 2002.
30. Obayahsi, S. and Sasaki, D., "SELF-ORGANIZING MAP OF PARETO SOLUTIONS OBTAINED FROM MULTIOBJECTIVE SUPERSONIC WING DESIGN," AIAA-Paper 2002-0991, Jan. 2002.
31. Yang, G., Kondo, M., and Obayashi, S., "Multiblock Navier-Stokes Solver for Wing/Fuselage Transport Aircraft," JSME International Journal, Series B, Vol. 45, No. 1, pp. 85-90, February 2002.
32. Sasaki, D., Yang, G. and Obayashi, S., "Multiobjective GA for SST Wing-Body Shape Design," Proceedings of Parallel CFD 2002, May, 2002.
33. Kanazaki, M., Obayashi, S. and Nakahashi K.,　"EXHAUST MANIFOLD DESIGN FOR A CAR ENGINE BASED ON ENGINE CYCLE SIMULATION," Parallel Computational Fluid Dynamics International Conference Parallel CFD 2002, May, 2002.
34. Kanazaki, M., Obayashi, S. and Nakahashi, K., "Effects of Nacelle Floes on SST Wing-Body Configuration Computed by Unstructured Euler Solver," the 4th GRACM Congress on Computational Mechanics, June, 2002.
35. Sasaki, D., Obayashi, S., and Nakahashi, K., "Navier-Stokes Optimization of Supersonic Wings with Four Objectives Using Evolutionary Algorithm," Journal of Aircraft, Vol. 39, No. 4, pp. 621-629, July-August 2002.
36. Sasaki, D. Yang, G. and Obayashi, S., "Automated Aerodynamic Shape Optimization System for SST Wing-Body Configuration," AIAA 2002-5549, September, 2002.
37. Kanazaki, M., Obayashi, S. Morikawa, M. and Nakahashi K., "Multiobjective Design Optimization of Merging Configuration for an Exhaust Manifold of a Car Engine," PPSN, the 7th international conference on parallel problem solving from nature, p.p.281-287, September, 2002.
38. YANG, G., OBAYASHI, S. and NAKAMICHI, J., "AILERON FLUTTER CALCULATION FOR A SUPERSONIC FUSELAGE-WING CONFIGURATION," invited paper, 23rd Congress of the International Council of the Aeronautical Sciences, CD-ROM, September, 2002
39. Yamazaki, W., Sasaki, D., Obayashi, S., Matsushima, K. and Nakahashi, K., "Aerodynamic Optimization of Supersonic Transport at Near-Sonic Region," Proceedings of Engin Soft & modeFRONTIER Conference and user's meeting 2002.
40. Sasaki, D. and Obayashi, S., "Datamining from Pareto Solutions of Supersonic Wing-Fuselage Shape Design," Proceedings of CJK-OSM2, pp.719-724, November, 2002.
41. Sasaki, D., Obayashi, S. and Nakahashi, K., "Navier-Stokes Optimization of Supersonic Wings with Four Objectives Using Evolutinary Algorithm" Journal of Aircraft, Vol.39, No.4, pp.621-629, 2003.
42. Daisuke Sasaki, Guowei Yang, Shigeru Obayashi, "Automated Aerodynamic Optimization System for SST Wing-Body Configuration," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.46, No.154, pp.230-237, 2004.
43. Guru P. Guruswamy and Shigeru Obayashi, "Study on the Use of High-Fidelity Methods in Aeroelastic Optimization", Journal of Aircraft, Vol. 41, No. 3, pp. 616-619, May-June 2004.
44. Shigeru OBAYASHI, Daisuke SASAKI and Akira OYAMA, "Finding Tradeoffs by Using Multiobjective Optimization Algorithms", Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 47, No. 155, pp. 51-58, MAY 2004.
45. A. Oyama, M.-S. Liou, S. Obayashi, "Transonic Axial-Flow Blade Optimization:　Evolutionary Algorithms/Three-Dimensional Navier-Stoke Solver," JOURNAL OF PROPULSION AND POWER, Vol. 20, No. 4, pp. 612-619. July-August 2004.
46. Daisuke Sasaki and Shigeru Obayash, "Efficient Search for Trade-Offs by Adaptive Range Multi-Objective Genetic Algorithms," Journal of Aerospace Computing, Information, and Communication, vol. 2, no. 1, 2005, pp. 44-64.
47. Shigeru Obayashi and Daisuke Sasaki, "Multiobjective Aerodynamic Design and Visualization of Supersonic Wings by Using Adaptive Range Multiobjective Genetic Algorithms (chapter 13)," Coello Coello and Lamont (eds.), Applications of Multi-Objective Evolutionary Algorithms, World Scientific Publishing, New Jersey, 2004.
48. Lucia PARUSSINI, Valentino PEDIRODA and Shigeru OBAYASHI, "Design under Uncertainties of Wings in Transonic Field," JSME International Journal Series B, Special Issue on Advanced Fluid Information, Vol. 48, No. 2, May 2005, pp.218-223.
49. Sinkyu JEONG, Shigeru OBAYASHI, Kazuomi YAMAMOTO, "Aerodynamic Optimization Design with Kriging Model," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.48 ,No.161, November, 2005, pp.161-168
50. Shinkyu Jeong, Sasaki Daisuke and Shigeru Obayashi,　 "Knowledge Discovery in Aerodynamic Design Space using Data Mining," The Korean Society for Aeronautical and Space Sciences, Vol.34 ,No.1,　January, 2006, pp.49-55.
51. Shinkyu Jeong, Kazuomi Yamamoto and Shigeru Obayashi, "A Kriging Model-Based Probabilistic Optimization Method with an Adaptive Search Region," Engineering Optimization, Vol. 38, 2006, pp. 541-555.
52. Shinkyu Jeong and Shigeru Obayashi,　"Multi-Objective Optimization Using Kriging Model and Data Mining ," KSAS International Journal , Vol.7, No. 1, 2006, May, pp.1-12.
53. K. Chiba, S. Obayashi, K. Nakahashi,　 "Design Exploration of Aerodynamic Wing Shape for Reusable Launch Vehicle Flyback Booster,"Journal of Aircraft, Vol.43, No. 3, May-June 2006, pp. 832-836.
54. Shinkyu Jeong, Youichi Minemura and Shigeru Obayashi, "Optimization of Combustion Chamber for Diesel Engine Using Kriging Model," Journal of Fluid Science and Technology, Vol.1, 2006, pp.138-146.
    
    

© copyright 2003-2007 Obayashi Lab. All Right Reserved