[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Sasaki et al., 2001 - Google Patents

Evolutionary algorithm vs. adjoint method applied to sst shape optimization

Sasaki et al., 2001

View PDF
Document ID
13324181831112036947
Author
Sasaki D
Obayashi S
Kim H
Publication year
Publication venue
The Annual Conference of CFD Society of Canada, Waterloo

External Links

Snippet

CFD techniques have been improved for higher reliability and higher accuracy recently. As a result, CFD has been integrated into aerodynamic optimization. Automated aerodynamic optimization is expected to reduce time and cost of aircraft design. In the aerodynamic …
Continue reading at www.ifs.tohoku.ac.jp (PDF) (other versions)

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50—Computer-aided design
    • G06F17/5009—Computer-aided design using simulation
    • G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/30—Information retrieval; Database structures therefor; File system structures therefor
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06N—COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS
    • G06N3/00—Computer systems based on biological models
    • G06N3/02—Computer systems based on biological models using neural network models

Similar Documents

Publication Publication Date Title
Obayashi et al. Multiobjective evolutionary computation for supersonic wing-shape optimization
Lindsay et al. A particle method and adaptive treecode for vortex sheet motion in three-dimensional flow
Reuther et al. Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation
Brezillon et al. 2D and 3D aerodynamic shape optimisation using the adjoint approach
Du et al. Aerodynamic inverse design using multifidelity models and manifold mapping
Obayashi et al. Multiobjective genetic algorithm applied to aerodynamic design of cascade airfoils
Nadarajah et al. Sonic boom reduction using an adjoint method for wing-body configurations in supersonic flow
CN104750948B (en) The optimization method of many extreme value multiple constraint problems in a kind of process Flight Vehicle Design
Yanhui et al. Performance improvement of optimization solutions by POD-based data mining
Sasaki et al. Aerodynamic shape optimization of supersonic wings by adaptive range multiobjective genetic algorithms
Chu et al. Reliability based optimization with metaheuristic algorithms and Latin hypercube sampling based surrogate models
Sasaki et al. Evolutionary algorithm vs. adjoint method applied to sst shape optimization
Sasaki et al. Multiobjective aerodynamic optimization of supersonic wings using Navier-Stokes equations
Anand et al. Deep Learning Framework for Design and Optimization of Rotor Blades
Koc et al. Aerodynamic design of wing-body-nacelle-pylon configuration
Rasheed An incremental-approximate-clustering approach for developing dynamic reduced models for design optimization
Sasaki et al. Navier-Stokes optimization of supersonic wings with four design objectives using evolutionary algorithm
Vaglio-Laurin On the PLK method and the supersonic blunt-body problem
Obayashi et al. Design optimization of supersonic wings using evolutionary algorithms
Yang et al. Response surface technique for static aeroelastic optimization on a high-aspect-ratio wing
Blasi et al. Particle swarm approach in finding optimum aircraft configuration
Jameson et al. Euler calculations for a complete aircraft
Zhu et al. Multi-objective optimization design of airfoil and wing
Takahashi et al. Inverse optimization of transonic wing shape for mid-size regional aircraft
Ahn et al. Two-point design optimization of transonic airfoil using response surface methodology