Chiba, K., Kanazaki, M., Nakamiya, M., Kitagawa, K., and Shimada, T., Conceptual Design of Single-Stage Launch Vehicle with Hybrid Rocket Engine for Scientific Observation Using Design Informatics, Journal of Space Engineering, Vol.6, No.1, 2013, pp.15-27.
Takii, K., Kanazaki, M., Ishiko, K., Hayashi, K., Hashimoto, A., and Aoyama, T., “Unsteady Numerical Simulations of HTV-R Reentry Capsule by Using Detached-Eddy Simulation,” AIAA Scitech2014, 52nd Aerospace Sciences Meeting (AIAA), AIAA 2014-0249, Washington D. C., U. S. A., January 2014.
OTHMAN, N., and Kanazaki, M., "PREDICTION OF AERODYNAMIC COEFFICIENTS AND DERIVATIVES BY SURROGATE MODEL APPROACH", ASIA-PACIFIC INTERNATIONAL CONGRESS ON ENGINEERING & NATURAL SCIENCES (APICENS) 2013, [CDROM], Taipei, December, 2013.
Nakayama, Y., Kanazaki, M., Yotsuya, Y., and Matsushima, K., "Design of Novel Wing Body Considering Intake/Exhaust Effects," The 2013 Asia-Pacific International Symposium on Aerospace Texhnology (APISAT-2013), 03-01-1, Takamatsu Japan, 2013.
Fumio KANAMORI, Yosuke KITAGAWA, Masaki NAKAMIYA, Koki KITAGAWA, Masahiro KANAZAKI and Toru SHIMADA, "Conceptual Design: Dependence of Parameterization on Design Performance of Three Stage Hybrid Rocket," Tenth International Conference on Flow Dynamics (ICFD2013), [USB], Sendai Japan, 2013.
Sato, T., Kanazaki, M., Yotsuya, Y., and Matsushima, K., "Parametric Airfoil Representation Toward Efficient Design Knowledge Discovery in Various Flow Condition," The 2013 Asia-Pacific International Symposium on Aerospace Texhnology (APISAT-2013), 03-01-1, Takamatsu Japan, 2013.
Kazuhisa Chiba, Masahiro Kanazaki, Masaki Nakamiya, Koki Kitagawa and Toru Shimada. Conceptual Design of Single-Stage Launch Vehicle with Hybrid Rocket Engine for Scientific Observation Using Design Informatics, in Evolutionary and Deterministic Methods for Design, Optimization and Control with Applications to Industrial and Societal Problems (EUROGEN 2013), pp. 49--52, ULPGC, Las Palmas de Gran Canaria, Spain, October 7-9, 2013.
Takashi Matsuno,Kengo Maeda,Gouji Yamada,Hiromitsu Kawazo,Masahiro Kanazaki, "Improvement of Flow Control Performance of Plasma Actuator Using Wind-Tunnel Test Based Efficient Global Optimization,"43rd AIAA Fluid Dyanmics Conference, 2013.
Kanazaki, M., Matsuno, T., Maeda, K., and Kawazaoe, "Wind Tunnel Evaluation?Based Optimization for Improvement of Flow Control by Plasma Actuator using Kriging Model-Based Genetic Algorithm," The annual IEEE Congress on Evolutionary Computation, Cancun Mexico, June 2013.
Hidehiro Takagi，Yoshikazu Makino，Masahiro Kanazaki "Mixed-Fidelity Efficient Global Optimization Applied to Design of Supersonic Wing,"APCATS’2013, July, 2013.
Mashiro Kanazaki, "Efficient Design Exploration for Civil Aircraft Using a Kriging-Based Genetic," EUROGEN 2013, Spain, October 7th-9th, 2013.
Kanazaki, M., Matsuno, T., Maeda, K., and Kawazaoe,Efficient Global Optimization Applied to Wind Tunnel Evaluation Based Optimization for Improvement of Flow Control by Plasma Actuator, "Japan-Finland Joint Seminar, Muroran, June 2013.