A Study of the CST Parameterization Characteristics
暂无分享,去创建一个
[1] Patrice Castonguay,et al. SURVEY OF SHAPE PARAMETERIZATION TECHNIQUES AND ITS EFFECT ON THREE-DIMENSIONAL AERODYNAMIC SHAPE OPTIMIZATION , 2007 .
[2] Luis Santos,et al. Inverse aerodynamic design applications using the MGM hybrid formulation , 2009 .
[3] S. Obayashi,et al. Aerodynamic Optimization of Supersonic Transport Wing Using Unstructured Adjoint Method , 2001 .
[4] Raymond M. Hicks,et al. Wing design by numerical optimization , 1977 .
[5] Antony Jameson,et al. Reduction of the Adjoint Gradient Formula in the Continuous Limit , 2003 .
[6] Antony Jameson,et al. Reduction of the Adjoint Gradient Formula for Aerodynamic Shape Optimization Problems , 2003 .
[7] John E. Bussoletti,et al. "Fundamental" Parameteric Geometry Representations for Aircraft Component Shapes , 2006 .
[8] Kazuhiro Nakahashi,et al. Unstructured adjoint method for Navier-Stokes equations , 2005 .
[9] João Luiz F. Azevedo,et al. A Framework for Aerodynamic Optimization Based On Genetic Algorithms , 2009 .
[10] B. Kulfan. Universal Parametric Geometry Representation Method , 2008 .
[11] B. Kulfan. A Universal Parametric Geometry Representation Method - "CST" , 2007 .
[12] Patrice Castonguay,et al. Effect of Shape Parameterization on Aerodynamic Shape Optimization , 2007 .
[13] Brenda Kulfan. Recent Extensions and Applications of the "CST" Universal Parametric Geometry Representation Method , 2007 .
[14] Rida T. Farouki,et al. Legendre-Bernstein basis transformations , 2000 .