Survey of shape parameterization techniques for high-fidelity multidisciplinary shape optimization

被引:242
作者
Samareh, JA [1 ]
机构
[1] NASA, Langley Res Ctr, Multidisciplinary Optimizat Branch, Hampton, VA 23681 USA
关键词
D O I
10.2514/2.1391
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A survey is provided of shape parameterization techniques for multidisciplinary optimization, and some emerging ideas are highlighted. The survey focuses on the suitability of available techniques for multidisciplinary applications of complex configurations using high-fidelity analysis tools such as computational fluid dynamics and computational structural mechanics. The suitability criteria are based on the efficiency, effectiveness, ease of implementation, and availability of analytical sensitivities for geometry and grids. A section on sensitivity analysis, grid regeneration, and grid deformation techniques is also provided.
引用
收藏
页码:877 / 884
页数:8
相关论文
共 71 条
[1]  
ANDERSON KW, 1999, 993294 AIAA
[2]  
Anderson W. K., 1997, 970643 AIAA
[3]  
[Anonymous], TM86382 NASA
[4]  
Barr A. H., 1984, Computers & Graphics, V18, P21
[5]   UNSTEADY EULER AIRFOIL SOLUTIONS USING UNSTRUCTURED DYNAMIC MESHES [J].
BATINA, JT .
AIAA JOURNAL, 1990, 28 (08) :1381-1388
[6]  
BAYSAL O, 1998, 7 AIAA USAF NASA ISS, P1483
[7]   A SHAPE OPTIMIZATION APPROACH BASED ON NATURAL DESIGN VARIABLES AND SHAPE FUNCTIONS [J].
BELEGUNDU, AD ;
RAJAN, SD .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1988, 66 (01) :87-106
[8]  
BIEDRON RT, 1999, 1998 COMP AER WORKSH, P219
[9]   Adifor 2.0: Automatic differentiation of Fortran 77 programs [J].
Bischof, C ;
Khademi, P ;
Mauer, A ;
Carle, A .
IEEE COMPUTATIONAL SCIENCE & ENGINEERING, 1996, 3 (03) :18-32
[10]  
Bischof CH, 1997, SOFTWARE PRACT EXPER, V27, P1427, DOI 10.1002/(SICI)1097-024X(199712)27:12<1427::AID-SPE138>3.0.CO