With the growth in computing power and the advances in computational techniques, the growing competitiveness in air-craft industry calls for an accurate, efficient, and robust tools for advanced aircraft shape design. The development of the future aviation industry needs to solve the key problems of multidisciplinary integrated design and provide a powerful de-sign method and tools for the design of new high-performance aircraft. This paper presents an automated digitalized inte-grated platform for aerodynamics synthetic design and assessment (DIPasda) for complex shape. Our goal is to present a new general-purpose robust and efficient optimization platform which is aimed at real-life constrained designs where the conventional design approaches complicated and time-consuming. The DIPasda system contains a collection of func-tional modules for performing design and optimization studies by means of numerical optimization schemes, geometry parameterization techniques, surrogate models, high-fidelity computational analysis tools for different disciplines and so on. By introducing the system architecture of the platform in detail, the main functional modules and the multi-objective optimization process, the flexibility of the system architecture design and the completeness of the functional modules are demonstrated. At last optimization tests is presented to show the system’s design optimization capability.
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