The invention discloses a parameterization method suitable for designing a non-axisymmetric laminar flow
nacelle. The parameterization method comprises the following steps: step 1, dividing a to-be-deformed
nacelle into calculation grids for numerical
simulation; 2, building a control frame on the surface of the
nacelle to be deformed, and arranging control points; Step 3, giving a displacement variation of the
control point according to a demand; 4, calculating the displacement variation of a calculation grid node on the surface of the nacelle to be deformed according to the
control point onthe surface of the nacelle to be deformed, the displacement variation of the
control point and the calculation grid node by utilizing a
radial basis function interpolation method; And 5, superposing the coordinates of the calculation grid nodes on the surface of the nacelle to be deformed and the displacement variation of the calculation grid nodes on the surface of the nacelle to be deformed to obtain the deformed nacelle. According to the method, the control framework of the surface of the nacelle to be deformed is built, the control points are arranged, the
radial basis function interpolation technology is adopted, and the laminar nacelle configuration after deformation is quickly and accurately calculated according to the displacement variation of the control points.