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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.

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