A New Approach for Multidisciplinary Design : Multi-Objective Design Exploration
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概要
- 論文の詳細を見る
- 一般社団法人日本機械学会の論文
- 2006-12-12
著者
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Obayashi Shigeru
Institute Of Fluid Science Tohoku University
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Obayashi Shigeru
Institute Of Engineering Mechanics Tsukuba University
関連論文
- Multi-Objective Design Exploration and Its Application to Regional-Jet Wing Design
- Aerodynamic Optimization Design with Kriging Model
- Shape Optimization of Fish Tail Propulsion with Hydro-Elastic Effects
- Experimental and Computational Studies of Low-Speed Aerodynamic Performance and Flow Characteristics around a Supersonic Biplane
- Automated Aerodynamic Optimization System for SST Wing-Body Configuration
- Finding Tradeoffs by Using Multiobjective Optimization Algorithms
- Stacking-sequence Optimization of Composite Wing For Improving Transonic Flutter Limit
- Multi-Objective Design Optimization of an Air Cleaner Fan Using Kriging Models
- Two-Point Implicit Scheme for Euler Equations
- Open-Type Separation on Delta Wings for Leading-Edge Bluntness
- Design under Uncertainties of Wings in Transonic Field(Advanced Fluid Information)
- A New Approach for Multidisciplinary Design : Multi-Objective Design Exploration
- Design Exploration into a Tire Noise Reduction Problem
- Knowledge Discovery in Multidisciplinary Design Space for Regional-Jet Wings Using Data Mining
- Multidisciplinary Design Exploration for Transonic Regional-Jet Wing Shape
- Multiblock Navier-Stokes Solver for Wing/Fuselage Transport Aircraft
- Kriging/RBF-Hybrid Response Surface Methodology for Highly Nonlinear Functions
- Implementation of visual data mining for unsteady blood flow field in an aortic aneurysm
- Aerodynamic Characteristics and Effects of Winglets of the Boomless Tapered Supersonic Biplane during the Starting Process
- Airport Terrain-Induced Turbulence Simulations Integrated with Weather Prediction Data
- Investigation of Data Exploration Method for Thermal-Fluid Simulation Results Using Proper Orthogonal Decomposition
- Development of a Sensitivity-Adjustable Three-Component Force Balance and Its Application to Wind Tunnel Testing
- Preface
- Foreword(Advanced Fluid Information)
- Measurement of Aircraft Wake Vortices Using Doppler LIDAR
- Optimization of Combustion Chamber for Diesel Engine Using Kriging Model
- Assimilation Experiment of Lidar Measurements for Wake Turbulence