Extended 3D Class/Shape Transformation equations for multicomponent aircraft assemblies

[1]  Christian B Allen,et al.  High‐fidelity aerodynamic shape optimization of modern transport wing using efficient hierarchical parameterization , 2010 .

[2]  Brenda M. Kulfan,et al.  New Supersonic Wing Far-Field Composite-Element Wave-Drag Optimization Method , 2009 .

[3]  Aditi Chattopadhyay,et al.  Application of shape memory alloy (SMA) spars for aircraft maneuver enhancement , 2002, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[4]  Darren J. Hartl,et al.  Aero-structural optimization of shape memory alloy-based wing morphing via a class/shape transformation approach , 2018 .

[5]  Atsushi Ueno,et al.  Multi-fidelity low-boom design based on near-field pressure signature , 2016 .

[6]  Brenda Kulfan.  Recent Extensions and Applications of the "CST" Universal Parametric Geometry Representation Method , 2007 .

[7]  Peter G. Coen,et al.  Origins and Overview of the Shaped Sonic Boom Demonstration Program , 2005 .

[8]  Ce Yang,et al.  An airfoil parameterization method for the representation and optimization of wind turbine special airfoil , 2015 .

[9]  Sarah F. Frisken.  Efficient Curve Fitting , 2008, J. Graph. Tools.

[10]  Jean-Yves Trbpanier,et al.  Wing Aerodynamic Design Using an Optimized NURBS Geometrical Representation , 2000 .

[11]  Daisuke Sasaki,et al.  Multiobjective evolutionary computation for supersonic wing-shape optimization , 2000, IEEE Trans. Evol. Comput..

[12]  Darren J. Hartl,et al.  Structurally Consistent Class/Shape Transformation Equations for Morphing Airfoils , 2019, Journal of Aircraft.