Recent progress in aerodynamic design optimization

被引：2

作者：

Melvin, RG ^{[1
]}

Huffman, WP ^{[1
]}

Young, DP ^{[1
]}

Johnson, FT ^{[1
]}

Hilmes, CL ^{[1
]}

Bieterman, MB ^{[1
]}

机构：

[1] Boeing Co, Seattle, WA 98124 USA

来源：

INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS | 1999年 / 30卷 / 02期

关键词：

aerodynamic design optimization; multipoint design; aeroelastics;

D O I：

10.1002/(SICI)1097-0363(19990530)30:2<205::AID-FLD827>3.0.CO;2-U

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

Recent emphasis on reduction of design cycle time and cost in the design of commercial aircraft (P.E. Rubbert, 'CFD and the changing world of airplane design', AIAA Wright Brothers Lecture, September, 1994) has sparked a renewed interest in design optimization in aerodynamics, structures and aeroelastics. In this paper, recent developments in the use of design optimization in aerodynamics using the TRANAIR code are considered. Globalization techniques and the extension of the methodology to multipoint design will be discussed. Copyright (C) 1999 John Wiley & Sons, Ltd.

引用

页码：205 / 216

页数：12

共 13 条

[1]

BIETERMAN MB, 1994, BCSTECH94032

[2]

Bryson A. E., 1975, APPL OPTIMAL CONTROL

[3] INEXACT NEWTON METHODS [J].

DEMBO, RS ;

EISENSTAT, SC ;

STEIHAUG, T .

SIAM JOURNAL ON NUMERICAL ANALYSIS, 1982, 19 (02) :400-408

[4]

DRELA M, 1993, 930969 AIAA

[5]

Fletcher R., 1981, PRACTICAL METHODS OP

[6]

Gill M., 1981, Practical Optimization

[7]

Gill P E, 1986, USERS GUIDE LSSOL VE

[8]

GILL PE, 1986, SOL862 STANF U DEP O

[9]

Huffman W., 1993, 933111 AIAA

[10]

Jameson A., 1988, Journal of Scientific Computing, V3, P233, DOI 10.1007/BF01061285

← 1 2 →