@inproceedings{f8ff8f5ac5664bb18ea1ef99c0b4ead2,
title = "Co-evolutionary multiobjective multidisciplinary design optimization for the airframe/propulsion integration of hypersonic vehicles",
abstract = "To implement multidisciplinary design optimization (MDO) for the airframe/propulsion integration of hypersonic vehicles, this study provided a disciplinary design structure matrix based on the analysis of coupling relationships among disciplines. The decomposition and coordination strategies of the co-evolutionary method were used to decompose the coupling system for airframe/propulsion integration into multidisciplinary systems that were relatively independent and autonomous. The system level optimization model and disciplinary optimization models for airframe/propulsion integration were established. The multi-objective multidisciplinary problem of airframe/propulsion integration for a hypersonic vehicle was analyzed by employing the co-evolutionary multi-objective optimization algorithm. This yielded a satisfactory pareto optimal solution set and offers guidance for the overall design of hypersonic vehicles.",
author = "Dong Zhang and Shuo Tang",
note = "Publisher Copyright: {\textcopyright} 2015, American Institute of Aeronautics and Astronautics. All rights Reserved.; 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015 ; Conference date: 06-07-2015 Through 09-07-2015",
year = "2015",
doi = "10.2514/6.2015-3667",
language = "英语",
isbn = "9781624103209",
series = "20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015",
publisher = "AIAA American Institute of Aeronautics and Astronautics",
booktitle = "20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015",
}