主要介绍了结构/非结构混合CFD软件HyperFLOW的设计开发与验证。HyperFLOW软件在结构网格上采用结构算法,在非结构网格上采用非结构算法,以充分利用两种网格及解算器的优点。首先介绍了软件的体系结构和基本算法,然后采用NASA Trap-Wing高升力外形和DLR-F6翼身组合体,对软件的结构解算器和非结构解算器进行了验证。结果表明,该软件的结构解算器和非结构解算器均有较好的网格收敛性,计算结果与其他参考结果和试验数据均符合较好,具有可接受的可信度。 This paper mainly introduces the design, development and verification of HyperFLOW, a hybrid structured / unstructured CFD software. HyperFLOW software uses structural algorithms on structural grids and unstructured algorithms on unstructured grids to take full advantage of both grids and solvers. Firstly, the architecture and basic algorithms of the software are introduced. Then the structure solver and unstructured solver of the software are validated by NASA Trap-Wing high-lift profile and DLR-F6 wing-body combination. The results show that both the structure solver and the unstructured solver have good grid convergence. The calculated results are in good agreement with other reference and experimental data and have acceptable credibility.