研究提出控制学科在回路的多学科设计优化方法。
In this paper, multidisciplinary design optimization method with control discipline in the loop is studied.
针对层级系统的优化设计问题，研究了多学科层级协调优化方法。
This paper studied multidisciplinary hierarchic compatibility design optimization method for design of hierarchic system.
算例结果表明，本方法提供了一种对翼型既可作气动优化设计亦可进行多学科综合设计的有效工具。
Numerical results show that the present method is an effective and robust tool for designing or revising airfoils, as well as for multi disciplinary optimization.
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