SURVEY OF SHAPE PARAMETERIZATION TECHNIQUES AND ITS EFFECT ON THREE-DIMENSIONAL AERODYNAMIC SHAPE OPTIMIZATION
By Siva K. Nadarajah, Patrice Castonguay, A. Mousavi. 2007
94 citations recorded by the source corpus.
Subfields: Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/30cea78065e5fcc6e91baa6e7cc2441e79b540ed
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In Computational Mechanics
- Christian B. Allen
- Thomas C. S. Rendall
- A. Morris
- Xiaocong Han
- Daniel J. Poole
- Ning Qin
- Fengxia Zhu
- David W. Zingg
Citations in the corpus
- Metric-Based Mathematical Derivation of Efficient Airfoil Design Variables (2015, unknown): “[26].”
- An adaptive geometry parametrization for aerodynamic shape optimization (2014, background): “There exist a large variety of parametrization methods for aerodynamic applications (Samareh 2001; Castonguay and Nadarajah 2007; Nadarajah et al 2007).”
- Intuitive Class/Shape Function Parameterization for Airfoils (2014, methodology): “The Bezier polynomial and B-spline methods are widely used parameterization methods in aerodynamic design parameterization [1,6,7,8–10].”
- Domain-Element Method for Aerodynamic Shape Optimization Applied to a Modern Transport Wing (2009, background): “Awide variety of shape control andmorphingmethods have been developed [1–11], but these often do not allow sufficiently free-form design, can produce infeasible shapes, and do not allow the possibility of manual manipulation of the geometry [12,13].”