In this study the flowfield of vertical take-off landing (VTOL) military airplane working on the rough ground is simulated by numerical simulation The κ-ε turbulence model is adopted and the control-volume integration for finite difference associated with SIMPLEST algorithm are employed to simulate the three-dimensional, high-temperature and high-pressure flowfield. The effects of block, crossflow and impinging angle on the flowfield are discussed one by one in this paper. The velocity of upwash fountain is decreased when the distance between the two plates is less than 3D. The stagnation line distorted with crossflow and the strength of upwash fountain become weaken with blocks. The inward jets will enhance the upwash fountain, and decreasing the pressure and the temperature. On the contrary, the outward jets will decline the upwash fountain, whereas increasing the pressure and the temperature. In summary, the variation of parameters, such as crossflow, block, and impinging angle is strongly correlated with the upwash fountain and the flowfield structure.