Hybrid Optimization Design of Natural-Laminar-Flow(NLF) Supercritical Airfoil and Infinite Swept Wing
暂无分享,去创建一个
[1] David Hue,et al. Experimental and Numerical Methods for Transition and Drag Predictions of Laminar Airfoils , 2015 .
[2] S. Obayashi,et al. Genetic optimization of target pressure distributions for inverse design methods , 1996 .
[3] Antony Jameson,et al. Natural-Laminar-Flow Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction , 2009 .
[4] Zhong-Hua Han,et al. A Preconditioned Multigrid Method for Efficient Simulation of Three-dimensional Compressible and Incompressible Flows , 2007 .
[5] J. Crouch,et al. Boundary-Layer Transition Prediction for Laminar Flow Control (Invited) , 2015 .
[6] Geza Schrauf,et al. LARGE-SCALE LAMINAR FLOW TESTS EVALUATED WITH LINEAR STABILITY THEORY , 2001 .
[7] Hyoung-Jin Kim,et al. Aerodynamic Design of Transonic Wings Using the Target Pressure Optimization Approach , 1998 .
[8] Timothy W. Simpson,et al. Design and Analysis of Computer Experiments in Multidisciplinary Design Optimization: A Review of How Far We Have Come - Or Not , 2008 .
[9] Zhong-Hua Han,et al. Numerical Study of High-Resolution Scheme Based on Preconditioning Method , 2008 .
[10] Oh-Hyun Rho,et al. Inverse Design of Transonic Wings Using Wing Planform and Target Pressure Optimization , 2001 .
[11] S. Fu,et al. Supercritical natural laminar flow airfoil optimization for regional aircraft wing design , 2015 .