賀川祐太朗,渡邉真也,金崎雅博,依田 英之,千葉一永,「相関ルールに基づく非劣解分析システムのオンデマンド化」,進化計算学会論文誌,8 巻,2 号, p. 75-87,2018年2月.
Ariyarit, A., Kanazaki, M., "Multi-fidelity Multi-objective Efficient Global Optimization Applied to Airfoil Design Problems," Multidisciplinary Digital Publishing Institute, Vol. 7, Issue 12, 1318, Dec. 2017. (IF:1.7, doi:10.3390/app7121318)
Chiba, K., Kanazaki, M. and Shimada, T., "Simple control of oxidizer flux for efficient extinction-reignition on a single-stage hybrid rocket," Journal Aerospace Science and Technology, Elsevier, Vol. 71, p. p. 109-118, Dec. 2017. (IF2.057, doi: 10.1016/j.ast.2017.09.017)
Kanazaki, M., Yoda, H., Chiba, K., Kitagawa, K., and Shimada, T., "Conceptual Design Methodology of a Hybrid Rocket Engine-Powered Launch Vehicle for Sub-Orbital Flight," Journal of Aerospace Engineering, American Society of Civil Engineers, Volume 30 Issue 6, Nov. 2017. (IF0.839, doi: 10.1061/(ASCE)AS.1943-5525.0000778)
Kanazaki, M., Matsuno, T., Maeda, K. and Kawazoe, H., "Optimum Driving Condition for Lift Creating Cylinder by Plasma Actuators Based on Wind Tunnel Evaluation Based Design," International Journal of Mechanical Systems, Vol. 1, pp. 32-43, Oct. 2017. (doi: 10.1504/IJAL.2016.074913)
Ariyarit, A., Kanazaki, M., Tanabe, "Hybrid surrogate-model-based multi-fidelity efficient global optimization applied to helicopter blade design," Engineering Optimization, Taylor&Francis, p. p. 1-25, September 2017.(IF1.728, http://dx.doi.org/10.1080/0305215X.2017.1367391)
岸祐希, 金崎雅博, 牧野好和, 松島紀佐,「設計探査法による超音速最適翼型の平面形依存性に関する考察」,日本機械学会論文集,Vol. 83,No. 849, p. 16-00454,2017年5月.
Kobayasi, K., Kanazaki, M., "Numerical Study on Charging Efficiency Improvement via Impellers Design Exploration for a Centrifugal Compressor," ICFD2017, Sendai, Nob. 2017.
Tomisawa, K., Fujita, K., Oyama, A., Nagai, H., and Kanazaki, M., "Mars Airplane Design for the Next Balloon Experiment and Its Aerodynamic Characteristics Using CFD," ICFD2017, Sendai, 2017.
Kanazaki, M., Yamada, Y., and Nakamiya, M., "Trajectory Optimization of a Satellite for Multiple Active Space Debris Removal Based on a Method for the Traveling Serviceman Problem," The 21st Asia Pacific Symposium on Intelligent and Evolutionary Systems (IES 2017), Ha Noi, Nov. 2017.
Kanazaki, M., and Ariyarit, M.,"Kriging Model Based Multi-Objective/ Multi-fidelity Global Optimization Applied to Aeronautical Design Problems," EUROGEN2017, Madrid, Spain, 2017.
Watanabe, A., Itoh, T., Kanazaki, M., and Chiba, K., "A Scatterplots Selection Technique for Multi-Dimensional Data Visualization Combining with Parallel Coordinate Plots," 21st International Conference Information Visualisation, London, UK., 11-14, July, 2017.
Iwafuji, H., Kanazaki, M., Fujikawa, T. and Yonemoto, K., "Numerical Simulation of Supersonic/Hypersonic Flow for TSTO's Staging Separation," The 31st International Symposium on Shock Waves, Nagoya, July, 2017.
Kanazaki, M., Yoda, H., Chiba, K., Kitagawa, K., and Shimada, T, "Performance Evaluation of Altering-intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket Using Multi-Disciplinary Optimization," 7th European Conference for Aeronautics and Space Sciences, Milan, Italy, 3-6th July, 2017.
Kishi, Y., Kitazaki, S., Ariyarit, A. Kanazaki, M. and Makino Y., “Planform Dependency of Optimum Supersonic Airfoil for Wing-Body-Nacelle Configuration Using Multi-Fidelity Design Optimization,” 35th AIAA Applied Aerodynamics Conference, Denver, Colorado, June 2017.