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
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| Published in | 日本機械学会論文集 Vol. 83; no. 849; p. 16-00454 |
|---|---|
| Main Authors | , , , |
| Format | Journal Article |
| Language | Japanese |
| Published |
一般社団法人 日本機械学会
2017
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| Subjects | |
| Online Access | Get full text |
| ISSN | 2187-9761 |
| DOI | 10.1299/transjsme.16-00454 |
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| Author | 牧野, 好和 金崎, 雅博 岸, 祐希 松島, 紀佐 |
|---|---|
| Author_xml | – sequence: 1 fullname: 岸, 祐希 organization: 首都大学東京 システムデザイン研究科 – sequence: 1 fullname: 金崎, 雅博 organization: 首都大学東京 システムデザイン研究科 – sequence: 1 fullname: 牧野, 好和 organization: 宇宙航空研究開発機構 航空技術部門 – sequence: 1 fullname: 松島, 紀佐 organization: 富山大学 工学部 |
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| References | Jones, D. Schonlau, M. and Welch, W. J., Efficient global optimization of expensive black-box function, Journal of Global Optimization, Vol. 13, Issue 4 (1998), pp. 455-492. Makino, M., Sonic boom ― Theory and Phenomena, Sangyo Tosho (2000) (in Japanese). Makino, Y., Makimoto, T., Ishikawa, H., Aerodynamic shape design for a low sonic boom flight test using stratospheric balloon (D-SEND), 48th Aircraft Symposium, 3E6(2010) (in Japanese). Jeong, S., Murayama, M. and Yamamoto, K., Efficient optimization design method using Kriging model, Journal of Aircraft, Vol.42, No.2 (2005), pp. 413-420. Seto, N., Makino, Y., Takatoya, T., Kanazaki, M., Multidisciplinary design optimization of silent supersonic transport with efficient optimization techniques, Journal of the Japan Society for Aeronautical and Space Sciences, Vol.59, No.686 (2011), pp.61-69 (in Japanese). Sturdza, P., Extensive supersonic natural laminar flow on the Aerion business jet, 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2007-685(2007). Kanazaki, M., Tanaka, K., Jeong, S. and Yamamoto, K., Multi-objective aerodynamic exploration of elements' setting for high-lift airfoil using Kriging model, Journal of Aircraft, Vol.44, No.3 (2007), pp. 858-864. Vassberg, J., DeHaan, M.A., Rivers, S.M., and Wahls, R.A., Development of a common research model for applied CFD validation studies, 26th AIAA Applied Aerodynamics Conference, Guidance, Navigation, and Control and Co-located Conferences, AIAA 2008-6919(2008). Hashimoto, A., Murakami, K., Aoyama, T., Yamamoto, K., Murayama, M. and Lahur, P., Drag prediction on NASA common research model using automatic hexahedra grid-generation method, Journal of Aircraft, Vol. 51, No. 4(2014), pp. 1172-1182. Ye, K., Orthogonal column latin hypercubes and their application in computer experiments, Journal of American Statistical Association, Vol.93, No.444 (1998), pp. 1430-1439. Einfelbt, B., On Godunov-type methods for gas dynamics, SIAM Journal on Numerical Analysis, Vol.25, No.2(1988), pp.294-318. Kishi, Y., Planform dependency of multi-point aerodynamic performance for supersonic wing, 51th Aircraft Symposium, 1B08 (2013) (in Japanese). Takeuchi, K., Matsushima, K., Kanazaki, M. and Kusunose, K., CFD analysis on sweep angles of the leading and trailing edges of a wing in a supersonic flow, Transactions of the JSME (in Japanese), Vol.81, No.827 (2015), DOI: 10.1299/transjsme.15-00037. Hashimoto, A., Murakami, K., Aoyama, T., Ishiko, K., Hishida, M., Sakashita, M. and Lahur, P., Development of unstructured CFD code "FaSTAR", The 28th Congress of the International Council of the Aeronautical Sciences, ICAS2012-2.11ST(2012). Hiroyasu, T., Miki, M. and Watanabe, S., Divided range genetic algorithm in multiobjective optimization problems, International Workshop on Emergent Synthesis (1999), pp. 57-66. Makino, Y. and Makimoto, T., Development of CAPAS, conceptual design tool for supersonic aircraft, 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008, 1E15(2008) (in Japanese). Yuhara, T., Rinoie, K., Feasibility study of hydrogen fueled supersonic transport, The Japan Society for Aeronautical and Space Science, Vol.9 (2010), pp.29-35 (in Japanese). Kanazaki, M., Yokokawa, Y., Murayama, M., Ito, T., Jeong, S. and Yamamoto, K., Nacelle chine installation based on wind-tunnel test using efficient global optimization, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 51, No. 173 (2008), pp. 146-150. Spalart, P. and Allmaras, S., A one-equation turbulence model for aerodynamic flows, 30th Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings, AIAA 1992-439(1992). Jones, R. T. and Cohen, D., High speed wing theory, PRINCETON UNIVERSITY PRESS (1960). |
| References_xml | – reference: Kanazaki, M., Tanaka, K., Jeong, S. and Yamamoto, K., Multi-objective aerodynamic exploration of elements' setting for high-lift airfoil using Kriging model, Journal of Aircraft, Vol.44, No.3 (2007), pp. 858-864. – reference: Yuhara, T., Rinoie, K., Feasibility study of hydrogen fueled supersonic transport, The Japan Society for Aeronautical and Space Science, Vol.9 (2010), pp.29-35 (in Japanese). – reference: Hashimoto, A., Murakami, K., Aoyama, T., Yamamoto, K., Murayama, M. and Lahur, P., Drag prediction on NASA common research model using automatic hexahedra grid-generation method, Journal of Aircraft, Vol. 51, No. 4(2014), pp. 1172-1182. – reference: Hiroyasu, T., Miki, M. and Watanabe, S., Divided range genetic algorithm in multiobjective optimization problems, International Workshop on Emergent Synthesis (1999), pp. 57-66. – reference: Einfelbt, B., On Godunov-type methods for gas dynamics, SIAM Journal on Numerical Analysis, Vol.25, No.2(1988), pp.294-318. – reference: Kanazaki, M., Yokokawa, Y., Murayama, M., Ito, T., Jeong, S. and Yamamoto, K., Nacelle chine installation based on wind-tunnel test using efficient global optimization, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 51, No. 173 (2008), pp. 146-150. – reference: Jeong, S., Murayama, M. and Yamamoto, K., Efficient optimization design method using Kriging model, Journal of Aircraft, Vol.42, No.2 (2005), pp. 413-420. – reference: Kishi, Y., Planform dependency of multi-point aerodynamic performance for supersonic wing, 51th Aircraft Symposium, 1B08 (2013) (in Japanese). – reference: Vassberg, J., DeHaan, M.A., Rivers, S.M., and Wahls, R.A., Development of a common research model for applied CFD validation studies, 26th AIAA Applied Aerodynamics Conference, Guidance, Navigation, and Control and Co-located Conferences, AIAA 2008-6919(2008). – reference: Jones, D. Schonlau, M. and Welch, W. J., Efficient global optimization of expensive black-box function, Journal of Global Optimization, Vol. 13, Issue 4 (1998), pp. 455-492. – reference: Makino, M., Sonic boom ― Theory and Phenomena, Sangyo Tosho (2000) (in Japanese). – reference: Ye, K., Orthogonal column latin hypercubes and their application in computer experiments, Journal of American Statistical Association, Vol.93, No.444 (1998), pp. 1430-1439. – reference: Makino, Y. and Makimoto, T., Development of CAPAS, conceptual design tool for supersonic aircraft, 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008, 1E15(2008) (in Japanese). – reference: Takeuchi, K., Matsushima, K., Kanazaki, M. and Kusunose, K., CFD analysis on sweep angles of the leading and trailing edges of a wing in a supersonic flow, Transactions of the JSME (in Japanese), Vol.81, No.827 (2015), DOI: 10.1299/transjsme.15-00037. – reference: Hashimoto, A., Murakami, K., Aoyama, T., Ishiko, K., Hishida, M., Sakashita, M. and Lahur, P., Development of unstructured CFD code "FaSTAR", The 28th Congress of the International Council of the Aeronautical Sciences, ICAS2012-2.11ST(2012). – reference: Seto, N., Makino, Y., Takatoya, T., Kanazaki, M., Multidisciplinary design optimization of silent supersonic transport with efficient optimization techniques, Journal of the Japan Society for Aeronautical and Space Sciences, Vol.59, No.686 (2011), pp.61-69 (in Japanese). – reference: Jones, R. T. and Cohen, D., High speed wing theory, PRINCETON UNIVERSITY PRESS (1960). – reference: Sturdza, P., Extensive supersonic natural laminar flow on the Aerion business jet, 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA 2007-685(2007). – reference: Spalart, P. and Allmaras, S., A one-equation turbulence model for aerodynamic flows, 30th Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings, AIAA 1992-439(1992). – reference: Makino, Y., Makimoto, T., Ishikawa, H., Aerodynamic shape design for a low sonic boom flight test using stratospheric balloon (D-SEND), 48th Aircraft Symposium, 3E6(2010) (in Japanese). |
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| SubjectTerms | Airfoil Cranked arrow wing Optimization Single tapered wing Supersonic wing design |
| Title | 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 |
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