Co-Evolutionary Multi-Objective Multidisciplinary Design Optimization For Hypersonic Vehicles

DOI

10.2991/cisia-15.2015.212How to use a DOI?

Keywords

airframe; propulsion; hypersonic vehicle; multidisciplinary; MDO

Abstract

Integrated design of airframe/propulsion of hypersonic vehicles is a problem of multi-objective multidisciplinary design optimization (MDO) for complex coupled systems in nature. In order to implement a MDO on airframe/propulsion integration, firstly the design structure matrix was established based on the analysis of coupling relationships among disciplines for airframe/propulsion integration; secondly, the system optimization model and disciplinary optimization models for airframe/propulsion integration were proposed; finally, simulations for the multi-objective multidisciplinary design optimization of airframe/propulsion integration of hypersonic vehicles were conducted by means of co-evolutionary method and a satisfactory Pareto optimal solution set was obtained.

Copyright

© 2015, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - D. Zhang
AU  - S. Tang
PY  - 2015/06
DA  - 2015/06
TI  - Co-Evolutionary Multi-Objective Multidisciplinary Design Optimization For Hypersonic Vehicles
BT  - Proceedings of the International Conference on Computer Information Systems and Industrial Applications
PB  - Atlantis Press
SP  - 784
EP  - 787
SN  - 2352-538X
UR  - https://doi.org/10.2991/cisia-15.2015.212
DO  - 10.2991/cisia-15.2015.212
ID  - Zhang2015/06
ER  -