2007
DOI: 10.1016/j.compfluid.2007.01.008
|View full text |Cite
|
Sign up to set email alerts
|

Accurate CFD driven optimization of lifting surfaces for wing-body configuration

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2009
2009
2018
2018

Publication Types

Select...
3
2

Relationship

0
5

Authors

Journals

citations
Cited by 6 publications
(1 citation statement)
references
References 21 publications
0
1
0
Order By: Relevance
“…References [17,[28][29][30]33,34] applied variants of discrete sensitivity approaches to optimize engineering problems. Epstein and Peigin [26] used Genetic Algorithm to optimize three-dimensional lifting surfaces for wing-body aircraft configuration. In all these classes of optimization, the functional sensitivity derivatives are directly coupled to the solution of a set of linear partial differential equations, i.e., the co-state equations and their boundary conditions that result from the variation of the augmented Lagrangian function [27,31,32].…”
Section: Variational Sensitivity Analysismentioning
confidence: 99%
“…References [17,[28][29][30]33,34] applied variants of discrete sensitivity approaches to optimize engineering problems. Epstein and Peigin [26] used Genetic Algorithm to optimize three-dimensional lifting surfaces for wing-body aircraft configuration. In all these classes of optimization, the functional sensitivity derivatives are directly coupled to the solution of a set of linear partial differential equations, i.e., the co-state equations and their boundary conditions that result from the variation of the augmented Lagrangian function [27,31,32].…”
Section: Variational Sensitivity Analysismentioning
confidence: 99%