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Robust design of natural laminar flow supercritical airfoil by multi-objective evolution method
Ke Zhao,
Zheng Hong Gao
, Jiang Tao Huang
航空学院
Northwestern Polytechnical University Xian
China Aerodynamics Research and Development Center
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探究 'Robust design of natural laminar flow supercritical airfoil by multi-objective evolution method' 的科研主题。它们共同构成独一无二的指纹。
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Engineering
Laminar Flows
100%
Airfoil
100%
Robust Design
100%
Mach Number
14%
High Reynolds Number
14%
Kriging Model
14%
Surrogate Model
14%
Turbulent Boundary Layer
14%
Search Algorithm
14%
Aerodynamic Characteristic
14%
Freeform Deformation
14%
Non-Dominated Sorting Genetic Algorithm II
14%
Non-Uniform Rational B-Splines
14%
Spline Basis Function
14%
Optimized Airfoil
14%