An Aerodynamic Design Method for Supersonic Natural Laminar Flow Aircraft

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Date: 2014-06-16 01:13:10 Fluid mechanics Boundary layer Laminar flow Multidisciplinary design optimization Kriging Mathematical optimization Drag Airfoil Shape optimization Aerodynamics Aerospace engineering Fluid dynamics		An Aerodynamic Design Method for Supersonic Natural Laminar Flow Aircraft Add to Reading List Source URL: www.desktop.aero Download Document from Source Website File Size: 3,63 MB Share Document on Facebook

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