The invention belongs to the technical field of pneumatic models of
turbomachinery, and particularly relates to a modeling method for an aerodynamic model of a
turbomachinery blade, which comprises the following steps of: S1, reading a three-dimensional
solid model of the blade, including a pressure surface, a
suction surface, a
front edge and a
tail edge; s2, performing grid topology on the pressure surface and the
suction surface to obtain
two grid surfaces, and generating the pressure surface and the
suction surface which do not have complete
directivity through node distribution on the grid surfaces; s3,
lofting the pressure surface and the suction surface which do not have the complete
directivity, and generating the pressure surface and the suction surface which have the
directivity; and S4, combining the pressure surface and the suction surface with directivity, and combining the pressure surface and the suction surface with the runner line to generate a geometric entity. According to the modeling method, the distribution of the
point set on each blade height section is replaced by the distribution of the grid nodes on the pressure surface and the suction surface, so that the aerodynamic model can be quickly established for the blade, and the modeling precision is high; and the
eye fatigue can be effectively relieved without
processing a large amount of data.