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

Lee et al., 2016 - Google Patents

Surrogate model based design optimization of multiple wing sails considering flow interaction effect

Lee et al., 2016

View PDF
Document ID
7344809648943150054
Author
Lee H
Jo Y
Lee D
Choi S
Publication year
Publication venue
Ocean Engineering

External Links

Snippet

The purpose of our study is to numerically analyze the aerodynamic characteristics of multiple wing sails which have three identical wing sails in a row and optimize their shape and operation conditions in terms of the flap length, deflection angle and angle of attack …
Continue reading at acml.gnu.ac.kr (PDF) (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/5018Computer-aided design using simulation using finite difference methods or finite element methods
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00Indexing scheme relating to computer aided design [CAD]
    • G06F2217/16Numerical modeling
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00Indexing scheme relating to computer aided design [CAD]
    • G06F2217/46Fuselage
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/10Complex mathematical operations

Similar Documents

Publication Publication Date Title
Lee et al. Surrogate model based design optimization of multiple wing sails considering flow interaction effect
Ghoreyshi et al. Reduced order unsteady aerodynamic modeling for stability and control analysis using computational fluid dynamics
Stern et al. Computational ship hydrodynamics: Nowadays and way forward
Dantas et al. Numerical analysis of control surface effects on AUV manoeuvrability
LeDoux et al. Study based on the AIAA aerodynamic design optimization discussion group test cases
Lanzetta et al. Advances in aerodynamic drag extraction by far-field methods
Jung et al. γ− R e θ t Spalart–Allmaras with Crossflow Transition Model Using Hamiltonian–Strand Approach
Jung et al. Turbulent and unsteady flows on unstructured line-based Hamiltonian paths and strands grids
Bianchi et al. A numerical model for the analysis of the locomotion of a cownose ray
Peters et al. On the construction of a mode based reduced order model for a moving store
Turnock et al. Directly coupled fluid structural model of a ship rudder behind a propeller
Stradtner et al. Introduction to AVT-351: Enhanced Computational Performance and Stability & Control Prediction for NATO Military Vehicles
Saetta et al. Identification of flowfield regions by machine learning
Tay et al. Biplane and tail effects in flapping flight
Tian et al. A viscous vorticity method for propeller tip flows and leading edge vortex
Duong et al. Fluid–structure coupling in time domain for dynamic stall using purely lagrangian vortex method
Jo et al. Aerodynamic design optimization of wing-sails
Ebrahimi et al. A comparative numerical study on the performances and vortical patterns of two bioinspired oscillatory mechanisms: undulating and pure heaving
Kagemoto et al. Force and power estimation in fish-like locomotion using a vortex-lattice method
Todorov Aerodynamic characteristics of airfoil with single plain flap for light airplane wing
Greve Non-viscous calculation of propeller forces under consideration of free surface effects
Makino et al. Aerodynamic analysis of NASA common research model by block-structured cartesian mesh
Jirásek et al. Application of Volterra functions to X-31 aircraft model motion
Sugar-Gabor Discrete adjoint-based simultaneous analysis and design approach for conceptual aerodynamic optimization
Williams et al. Shape Optimization for a Parametrically-Defined Hypersonic Glide Vehicle