Creative Flow Research Division

Research output

Research output per year 1980 2007 2008 2010 2011 2012 2013 2014 2015 2016 2017 2018 2019 2020 2021 2022 2023

• 606 Article
• 312 Conference contribution
• 38 Paper
• 38 Conference article
• 37 More
  • 15 Review article
  • 9 Chapter
  • 9 Editorial
  • 4 Comment/debate

Research output per year

Research output per year

Search results

• 2022

  A Software to Visualize, Edit, Model and Mesh Vascular Networks

  Decroocq, M., Lavoue, G., Ohta, M. & Frindel, C., 2022, 44th Annual International Conference of the IEEE Engineering in Medicine and Biology Society, EMBC 2022. Institute of Electrical and Electronics Engineers Inc., p. 2208-2214 7 p. (Proceedings of the Annual International Conference of the IEEE Engineering in Medicine and Biology Society, EMBS; vol. 2022-July).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Networks 100%
  • Vascular Network 80%
  • Application Software 60%
  • Simulation Mode 40%
  • Visualization 40%

• Composite Kernel Functions for Surrogate Modeling using Recursive Multi-Fidelity Kriging

  Palar, P. S., Parussini, L., Bregant, L., Shimoyama, K., Izzaturrahman, M. F., Baehaqi, F. A. & Zuhal, L. R., 2022, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-0506. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Kernel 100%
  • Kriging 88%
  • Functions 66%
  • Composite 66%
  • Recursive 22%
  2 Citations (Scopus)

• Modeling Non-Stationarity with Deep Gaussian Processes: Applications in Aerospace Engineering

  Izzaturrahman, M. F., Palar, P. S., Zuhal, L. R. & Shimoyama, K., 2022, AIAA SciTech Forum 2022. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-1096. (AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Gaussian Process 100%
  • Investigation 25%
  • International System of Units 25%
  • Standard 16%
  • Ability 16%

• Unsteady Flow Field on Wing Surface in Propeller Slipstream at Low Reynolds Number

  Ikami, T., Fujita, K. & Nagai, H., 2022, AIAA AVIATION 2022 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2022-3983. (AIAA AVIATION 2022 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Slipstream 100%
  • Wings 60%
  • Flow Field 50%
  • Surfaces 50%
  • Flow Distribution 50%
• 2021

  Aerodynamic characteristics of turbojav measured with 1-m magnetic suspension and balance system

  Okuizumi, H., Sasaki, K., Konishi, Y. & Obayashi, S., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-13 13 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Aerodynamic Characteristic 100%
  • Throwing 25%
  • Suspension 25%
  • Angle of Attack 12%
  • Air Flow 12%

• Aerotaxis and aerokinesis of Dictyostelium discoideum under hypoxic microenvironments

  Hirose, S., Rieu, J. P., Anjard, C., Cochet-Escartin, O., Kikuchi, H. & Funamoto, K., 2021, 43rd Annual International Conference of the IEEE Engineering in Medicine and Biology Society, EMBC 2021. Institute of Electrical and Electronics Engineers Inc., p. 1187-1190 4 p. (Proceedings of the Annual International Conference of the IEEE Engineering in Medicine and Biology Society, EMBS).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  Open Access

  • Oxygen Concentration 100%
  • Discoideum 85%
  • Dictyostelium discoideum 85%
  • Oxygen 57%
  • Concentration Gradient 42%
  1 Citation (Scopus)

• A new position and attitude measurement method for complex shape models with non-circular cross section in magnetic suspension and balance system

  Horiguchi, M., Saito, Y., Nonomura, T., Asai, K., Sawada, H., Konishi, Y., Okuizumi, H. & Obayashi, S., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-12 12 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Measurement 100%
  • Procedures 100%
  • Measurement Method 100%
  • Suspension 80%
  • Error 60%
  1 Citation (Scopus)

• An Optimization Study of Strake Implementation on a Spaceplane

  Al Fatih, M. H., Shimoyama, K. & Kamisori, K., 2021, AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2021-3039. (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Optimization 100%
  • Wings 100%
  • Leading Edge 100%
  • Flow Condition 50%
  • Optimum Design 50%

• EVALUATION OF NORMALIZATION METHODS IN A CEREBRAL ARTERY ATLAS FOR AUTOMATIC LABELING

  Jin, K., Kitamura, K., Mugikura, S., Mori, N., Ohta, M. & Anzai, H., 2021, Biomedical and Biotechnology. American Society of Mechanical Engineers (ASME), v005t05a034. (ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE); vol. 5).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Accuracy 100%
  • Volume 33%
  • Image Quality 16%
  • Length 16%
  • Magnetic Resonance Angiography 16%

• Experimental investigation on aerodynamic performance of coaxial rotor at low reynolds numbers

  Yamaguchi, A., Golani, R. S., Fujita, K. & Nagai, H., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-12 12 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Aerodynamics 100%
  • Performance 100%
  • Coefficients 100%
  • Crater 66%
  • Reynolds Number 66%

• Gaussian processes and support vector regression for uncertainty quantification in aerodynamics

  Palar, P. S., Zakaria, K., Zuhal, L. R., Shimoyama, K. & Liem, R. P., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-12 12 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Kriging 100%
  • Kernel 100%
  • Support Vector Regression 100%
  • Uncertainty Quantification 40%
  • Simulation Mode 40%
  2 Citations (Scopus)

• Permeable membrane wing characteristics at reynolds number order of 10,000

  Fujita, K., Takahashi, K. & Nagai, H., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-10 10 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Wings 100%
  • Dynamic Pressure 80%
  • Reynolds' Number 60%
  • Membrane 60%
  • Unmanned Aerial Vehicle 40%

• Response evaluation of cnttsp for detection of dynamic boundary layer transition in low-speed wind tunnel

  Ikami, T., Fujita, K., Nagai, H. & Yorita, D., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-10 10 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Boundary Layer Transition 100%
  • Wings 66%
  • Temperature Sensitive Paint 66%
  • Models 66%
  • Pitch 66%
  2 Citations (Scopus)

• Validation of sub-millimeter resolution pressure measurement on free flight model mach 1.5

  Gonzales, J. P., Kurihara, D., Sakaue, H., Jemcov, A. & Nagai, H., 2021, AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-9 9 p. (AIAA Scitech 2021 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Free Flight 100%
  • Computational Fluid Dynamics 80%
  • Pressure Sensitive Paints 60%
  • Transients 60%
  • Pressure Measurement 40%
• 2020

  Bayesian methods for multi-objective optimization of a supersonic wing planform

  Jim, T. M. S., Faza, G. A., Palar, P. S. & Shimoyama, K., 2020 Jul 8, GECCO 2020 Companion - Proceedings of the 2020 Genetic and Evolutionary Computation Conference Companion. Association for Computing Machinery, Inc, p. 1641-1643 3 p. (GECCO 2020 Companion - Proceedings of the 2020 Genetic and Evolutionary Computation Conference Companion).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Optimization 100%
  • Wing Planforms 66%
  • Gradient 66%
  • Sample 66%
  • Convergence 66%
  3 Citations (Scopus)

• Blade element theory coupled with cfd applied to optimal design of rotor for mars exploration helicopter

  Uwatoko, K., Kanazaki, M., Nagai, H., Fujita, K. & Oyama, A., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-11 11 p. (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Rotors 100%
  • Low Reynolds Number 66%
  • Helicopters 66%
  • Rotor Blade 66%
  • Evaluation 66%
  1 Citation (Scopus)

• Combined kriging surrogate model for efficient global optimization using the optimal weighting method

  Appriou, T. & Shimoyama, K., 2020 Jul 8, GECCO 2020 Companion - Proceedings of the 2020 Genetic and Evolutionary Computation Conference Companion. Association for Computing Machinery, Inc, p. 29-30 2 p. (GECCO 2020 Companion - Proceedings of the 2020 Genetic and Evolutionary Computation Conference Companion).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Kriging 100%
  • Simulation Mode 60%
  • Interpolation 40%
  • Sample Point 30%
  • Ordinary Regression 30%

• Data assimilation for clear air turbulence by upstream lidar observation

  Yoshimura, R., Yakeno, A., Obayashi, S., Misaka, T. & Kikuchi, R., 2020, AIAA AVIATION 2020 FORUM. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA AVIATION 2020 FORUM; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Data Assimilation 100%
  • Observation 100%
  • Optical Radar 50%
  • Line of Sight 50%
  • Wind Velocity 50%

• Deployable wing model using ancf and uvlm: Multibody dynamic simulation and wind tunnel experiment

  Otsuka, K., Wang, Y., Fujita, K., Nagai, H. & Makihara, K., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Wings 100%
  • Simulation 71%
  • Experiments 42%
  • Tunnels 42%
  • Wind 42%
  3 Citations (Scopus)

• Development and evaluation of PVA-H 3D printed blood vessel biomodels with several stiffness

  Kobayashi, N., Shimizu, Y., Nagano, R., Tupin, S. A., Ito, M. & Ohta, M., 2020, Biomedical and Biotechnology. American Society of Mechanical Engineers (ASME), V005T05A008. (ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE); vol. 5).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Models 100%
  • Hydrogel 66%
  • Mechanical Properties 33%
  • Blood Vessels 33%
  • Printers 33%

• Differential-Stiffness-Films-Laminated Pouch Motor

  Takahashi, I. & Fujita, K., 2020 Jan, Proceedings of the 2020 IEEE/SICE International Symposium on System Integration, SII 2020. Institute of Electrical and Electronics Engineers Inc., p. 1156-1162 7 p. 9026000. (Proceedings of the 2020 IEEE/SICE International Symposium on System Integration, SII 2020).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Stiffness 100%
  • Robotics 100%
  • Performance 100%
  • Rocket 100%
  • Deformation Mechanism 50%
  1 Citation (Scopus)

• Drag coefficients of circular cylinders with fineness ratios of less than 0.50 measured by 0.1 and 0.3 m magnetic suspension and balance systems

  Kuwata, M., Yokota, S., Sawada, H., Abe, Y., Yakeno, A., Nonomura, T., Asai, K. & Obayashi, S., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-10 10 p. (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Drag Coefficient 100%
  • Ratios 75%
  • Circular Cylinder 62%
  • Aerodynamic Drag 25%
  • Model Position 25%
  1 Citation (Scopus)

• Experimental and rans analysis of full mars airplane configurations

  Taniguchi, S., Oyama, A., Okamoto, M., Anyoji, M., Fujita, K. & Nagai, H., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, p. 1-14 14 p. (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Reynolds-Averaged Navier-Stokes 100%
  • Simulation 75%
  • Experiments 62%
  • Good Agreement 50%
  • Sideslip Angle 37%

• Gradient-enhanced universal kriging with polynomial chaos as trend function

  Zuhal, L. R., Zakaria, K., Palar, P. S., Shimoyama, K. & Liem, R. P., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Kriging 100%
  • Gradients 100%
  • Polynomial 71%
  • Chaos 71%
  • Functions 57%

• Measurement of boundary layer transition on oscillating airfoil using cnttsp in low-speed wind tunnel

  Ikami, T., Fujita, K., Nagai, H. & Yorita, D., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Boundary Layer Transition 100%
  • Temperature Sensitive Paints 100%
  • Low Speed 100%
  • Wind Tunnels 66%
  • Hysteresis 33%
  4 Citations (Scopus)

• Parametric study of mars helicopter for pit crater exploration

  Fujita, K., Karaca, H. & Nagai, H., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Crater 100%
  • Mars 100%
  • Design 100%
  • Motors 66%
  • Exploration 66%
  5 Citations (Scopus)

• Surface pressure measurements over a free flight object in a ballistic range facility using two-color pressure-sensitive paint

  Kurihara, D., Caucherty, S., Gonzales, J., Sakaue, H., Kiritani, H., Fujita, K. & Nagai, H., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Pressure Sensitive Paints 100%
  • Images 80%
  • Surface Pressure 40%
  • Facilities 40%
  • Measurement 20%
  3 Citations (Scopus)

• Transition detection methods in a pitch-sweep test by means of tsp using lifetime and intensity measurements

  Yorita, D., Lemarechal, J., Klein, C., Fujita, K. & Nagai, H., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Pitch 100%
  • Temperature Sensitive Paint 75%
  • Models 75%
  • Model 75%
  • Temperature Sensitive Paints 75%
  6 Citations (Scopus)

• Transonic flow field analysis of a free flight capsule using ballistic range

  Kiritani, H., Tanaka, N., Ohtani, K., Fujita, K. & Nagai, H., 2020, AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2020 Forum; vol. 1 PartF).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Capsule 100%
  • Flow Distribution 50%
  • Flow Field 50%
  • Shock 50%
  • Recompression 37%
  1 Citation (Scopus)

• Uncertainty quantification methods for evolutionary optimization under uncertainty

  Palar, P. S., Shimoyama, K. & Zuhal, L. R., 2020 Jul 8, GECCO 2020 Companion - Proceedings of the 2020 Genetic and Evolutionary Computation Conference Companion. Association for Computing Machinery, Inc, p. 1614-1622 9 p. (GECCO 2020 Companion - Proceedings of the 2020 Genetic and Evolutionary Computation Conference Companion).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Uncertainty Quantification 100%
  • Evolutionary Computation 33%
  • Optimization 22%
  • Roles 22%
  • Objective Function 11%
• 2019

  A multi-point mechanism of expected hypervolume improvement for parallel multi-objective Bayesian global optimization

  Yang, K., Palar, P. S., Emmerich, M., Shimoyama, K. & Bäck, T., 2019 Jul 13, GECCO 2019 - Proceedings of the 2019 Genetic and Evolutionary Computation Conference. Association for Computing Machinery, Inc, p. 656-663 8 p. (GECCO 2019 - Proceedings of the 2019 Genetic and Evolutionary Computation Conference).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Multiobjective 100%
  • Global Optimization 75%
  • Objective Space 75%
  • Algorithms 50%
  • Real World 50%
  12 Citations (Scopus)

• Development of free flight experimental and analytical procedures for atmospheric entry vehicles

  Jegede, O., Fujita, K., Nagai, H. & Tanno, H., 2019 Jan 1, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Free Flight 100%
  • Investigation 40%
  • Effort 40%
  • Damping Coefficient 40%
  • Linear Accelerometer 40%
  3 Citations (Scopus)

• Effects of rib number and rigid trailing edge on flexible-skinned thick wing at low reynolds number

  Fujita, K., Uechi, K., Takahashi, K. & Nagai, H., 2019 Jan 1, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Aerodynamic Characteristic 100%
  • Wings 83%
  • Membrane 33%
  • Deformation 33%
  • Trailing Edge 33%
  1 Citation (Scopus)

• Experimental study on high efficiency of aerodynamic performance of rotor blades for mars helicopter

  Kanou, K., Fujita, K. & Nagai, H., 2019 Jan 1, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Rotors 100%
  • Performance Test 42%
  • Aerodynamic Performance 42%
  • Helicopters 28%
  • Rotor Blade 28%
  2 Citations (Scopus)

• Experimental study on the effects of radial dispersion of spherical particles on the suspension rheology

  Kawaguchi, M., Fukui, T., Funamoto, K., Miyauchi, S. & Hayase, T., 2019, Multiphase Flow. American Society of Mechanical Engineers (ASME), (ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019; vol. 5).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Particle 100%
  • Suspension Rheology 50%
  • Microstructure 25%
  • Spherical Particle 25%
  • Velocity Field 25%
  2 Citations (Scopus)

• Flow field on wing surface with control surface in propeller slipstream at low reynolds number

  Ikami, T., Kanou, K., Takahashi, K., Fujita, K. & Nagai, H., 2019 Jan 1, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Slipstream 100%
  • Control Surfaces 40%
  • Wings 30%
  • Low Reynolds Number 30%
  • Surfaces 30%
  6 Citations (Scopus)

• Influence of input image configurations on output of a convolutional neural network to detect cerebral aneurysms

  Watanabe, K., Anzai, H., Juchler, N., Hirsch, S., Bijlenga, P. & Ohta, M., 2019, Biomedical and Biotechnology Engineering. American Society of Mechanical Engineers (ASME), (ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE); vol. 3).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Aneurysm 100%
  • Cerebral Aneurysm 80%
  • Convolutional Neural Network 80%
  • Brain Artery Aneurysm 80%
  • Computer 60%

• Kriging with composite kernel learning for surrogate modeling in computer experiments

  Palar, P. S. & Shimoyama, K., 2019 Jan 1, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Kernel 100%
  • Composite 63%
  • Kriging 54%
  • Surrogate Modeling 27%
  • Engineering Design Problem 18%
  3 Citations (Scopus)

• Multi-objective kriging-based optimization for high-fidelity wind turbine design

  Zuhal, L. R., Faza, G. A., Palar, P. S. & Shimoyama, K., 2019 Jan 1, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Wind Turbine 100%
  • Optimization 66%
  • Wind Turbine Design 66%
  • Volume 66%
  • Meshes 50%
  2 Citations (Scopus)

• On the use of metaheuristics in hyperparameters optimization of Gaussian processes

  Palar, P. S., Zuhal, L. R. & Shimoyama, K., 2019 Jul 13, GECCO 2019 Companion - Proceedings of the 2019 Genetic and Evolutionary Computation Conference Companion. Association for Computing Machinery, Inc, p. 263-264 2 p. (GECCO 2019 Companion - Proceedings of the 2019 Genetic and Evolutionary Computation Conference Companion).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Covariance Matrix 100%
  • Evolution Strategy 100%
  • Differential Evolution 100%
  • Gaussian Process 100%
  • Adaptation 100%
  2 Citations (Scopus)

• On the use of surrogate models in engineering design optimization and exploration: The key issues

  Palar, P. S., Zuhal, L. R., Liem, R. P. & Shimoyama, K., 2019 Jul 13, GECCO 2019 Companion - Proceedings of the 2019 Genetic and Evolutionary Computation Conference Companion. Association for Computing Machinery, Inc, p. 1592-1602 11 p. (GECCO 2019 Companion - Proceedings of the 2019 Genetic and Evolutionary Computation Conference Companion).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Surrogate Model 100%
  • Optimization 66%
  • Design Exploration 66%
  • Engineering Design 66%
  • Design Optimization 50%
  14 Citations (Scopus)

• Reentry capsule dynamic instability with different aft-body shape in transonic flow

  Nomura, M., Robbe, A., Fujita, K. & Nagai, H., 2019 Jan 1, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Oscillation 100%
  • Flow Distribution 75%
  • Model 75%
  • Differences 75%
  • Flow Field 75%
  3 Citations (Scopus)

• Stochastic re-entry trajectory analysis with uncertain initial conditions for safety assessment

  Tokunaga, A., Sotoguchi, A., Shimoyama, K. & Fujimoto, K., 2019 Jan 1, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Uncertainty Quantification 100%
  • Reentry Trajectories 66%
  • Trajectory Analysis 50%
  • Kinetic Energy 33%
  • Speed 33%

• The relationship between the arterial geometry and wall shear stress in the vertebrobasilar system

  Pan, F., Anzai, H., Mugikura, S., Kitamura, K. & Ohta, M., 2019, Biomedical and Biotechnology Engineering. American Society of Mechanical Engineers (ASME), (ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE); vol. 3).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Shear Stress 100%
  • Atherosclerosis 42%
  • Morphology 28%
  • Basilar Artery 28%
  • Artery Disease 28%

• Thermo-fluid dynamic design exploration of a double pipe heat exchanger

  Hirano, T., Yoshimura, M., Shimoyama, K. & Komiya, A., 2019, Computational Fluid Dynamics. American Society of Mechanical Engineers (ASME), (ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019; vol. 2).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Heat Transfer 100%
  • Shapes 83%
  • Performance 66%
  • Temperature 50%
  • Area 50%

• Three-dimensional global stability on stuart vortex of free shear layer

  Yakeno, A. & Hirota, M., 2019, Progress in Turbulence VIII - Proceedings of the iTi Conference in Turbulence 2018. Örlü, R., Talamelli, A., Peinke, J. & Oberlack, M. (eds.). Springer Science and Business Media, LLC, p. 9-13 5 p. (Springer Proceedings in Physics; vol. 226).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Turbulence 100%
  • Eddy 66%
  • Two Dimensional 33%
  • Free Shear Layer 33%
  • Generates 33%
  1 Citation (Scopus)
• 2018

  Aerodynamic analysis of NASA common research model by block-structured cartesian mesh

  Makino, S., Kojima, T., Misaka, T., Obayashi, S. & Sasaki, D., 2018, AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Buildings 100%
  • Turbulent Boundary Layer 100%
  • Flow Solver 50%
  • NASA 50%
  • Aerodynamic Analysis 50%
  2 Citations (Scopus)

• Aerodynamic characteristics of mars airplane airfoils with control surface in propeller slipstream

  Kurane, K., Uechi, K., Takahashi, K., Fujita, K. & Nagai, H., 2018, AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Slipstream 100%
  • Aerodynamic Characteristic 66%
  • Control Surfaces 50%
  • Aircraft 50%
  • Mars 50%
  5 Citations (Scopus)

• Aerodynamic design of airfoil for flying wing mars airplane

  Harada, T., Fujita, K., Oyama, A., Mamori, H. & Yamamoto, M., 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; vol. 0, no. 210059).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Aerodynamics 100%
  • Mars 75%
  • Performance 50%
  • Flow Distribution 25%
  • Stokes Flow 25%
  1 Citation (Scopus)

• Aerodynamic measurements of AGARD-B model at high angles of attack by 1-m magnetic suspension and balance system

  Senda, H., Sawada, H., Okuizumi, H., Konishi, Y. & Obayashi, S., 2018, AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018).

  Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

  • Angle-of-Attack 100%
  • Angle of Attack 100%
  • Models 85%
  • Model 85%
  • High Angle 71%
  7 Citations (Scopus)