The invention discloses a high-precision wind tunnel
nozzle profile design method, and belongs to the technical field of wind tunnel
nozzle profile design based on a computer. The problems that in the prior art, a traditional wind tunnel
nozzle molded surface design method is poor in process feasibility, and the number of molded surface correction iterations is large are solved. According to the method,
modeling software is adopted to construct an initial profile
mathematical model, geometric constraints are integrated, a wall thickness
initial distribution model is established, and wall thickness distribution is optimized; s2, quantizing an objective function according to the constraint and the
model parameters in the step S1, optimizing the objective function, and refining the constraint to obtain refined constraint conditions; and according to the wall thickness
initial distribution model and the wall thickness parameters,
design software is combined with the refined constraint conditions to carry out parametric modeling, a process feedback mechanism is constructed to carry out correction compensation on initial molded surface modeling, and high-precision wind tunnel nozzle molded surface design is completed. The pneumatic performance and the material
utilization rate are effectively improved, and the method can be applied to high-precision pneumatic
verification tests.