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Numerical biobjective optimal design of airfoil and wing

Zhu, Z. Q. ; Yu, R. X. LU orcid ; Fu, H. Y. and Chen, Y. C. (2003) In Journal of Aircraft 40(3). p.600-602
Abstract

Biobjective and bidisciplinary optimal design of high-performance airfoil and wing applying two kinds of optimization methods and genetic algorithm are discussed. An objective function combination method (OFCM) of constructing a resultant objective function in DOM or a fitness function in GA for biobjective optimization.

Please use this url to cite or link to this publication:
author
; ; and
publishing date
type
Contribution to journal
publication status
published
subject
keywords
Design, Structure (composition), Descending direction
in
Journal of Aircraft
volume
40
issue
3
pages
3 pages
publisher
American Institute of Aeronautics and Astronautics
external identifiers
  • scopus:0038204463
ISSN
0021-8669
language
English
LU publication?
no
id
a4fef292-a0d3-481d-b300-9758d54611dd
date added to LUP
2019-09-13 13:03:09
date last changed
2025-10-14 09:01:55
@article{a4fef292-a0d3-481d-b300-9758d54611dd,
  abstract     = {{<p>Biobjective and bidisciplinary optimal design of high-performance airfoil and wing applying two kinds of optimization methods and genetic algorithm are discussed. An objective function combination method (OFCM) of constructing a resultant objective function in DOM or a fitness function in GA for biobjective optimization.</p>}},
  author       = {{Zhu, Z. Q. and Yu, R. X. and Fu, H. Y. and Chen, Y. C.}},
  issn         = {{0021-8669}},
  keywords     = {{Design; Structure (composition); Descending direction}},
  language     = {{eng}},
  month        = {{05}},
  number       = {{3}},
  pages        = {{600--602}},
  publisher    = {{American Institute of Aeronautics and Astronautics}},
  series       = {{Journal of Aircraft}},
  title        = {{Numerical biobjective optimal design of airfoil and wing}},
  volume       = {{40}},
  year         = {{2003}},
}