The invention relates to a double-engine
propeller noise prediction and optimization method based on an analytical method, and belongs to the field of
aviation acoustics. The method disclosed by the invention comprises a
noise prediction method and a
noise optimization method, the noise prediction method establishes a noise prediction model based on an improved
propeller characteristic theory, and the
noise optimization method comprises the following steps: S1, establishing a noise objective function based on the noise prediction model, solving a first-order partial derivative and a Hessian matrix of the noise objective function, and obtaining a first-order partial derivative of the noise objective function; the method comprises the steps of S1, providing a noise target function, S2, providing a new Euler formula transformation method, and converting a triangular polynomial corresponding to a first-order partial derivative of the noise target function into a zero-equivalent algebraic polynomial, S3, analyzing and solving the zero point of the algebraic polynomial by using a Fourier-Frobenius
matrix method, and S4, realizing synchronous maximum
noise reduction control. According to the method, an improved
propeller characteristic value theory and a Hessian + Fourier-Frobenius
matrix method are used for rapidly and accurately solving an analytical solution of the minimum noise, and the method is combined with
synchronous control, so that the limitation on the time and precision of predicting the minimum noise is overcome.