The invention discloses a self-adaptive parameter identification method for an SST turbulence model in
shock wave boundary layer interference, and the method comprises the steps: S1, constructing a high-dimensional
sample space according to a closed parameter interval range of the SST turbulence model under a determined working condition, carrying out the optimal Latin
hypercube sampling, and uniformly obtaining the sample information in the whole space, and enabling the sample information to serve as an input parameter sample; s2, performing numerical
simulation based on an input parameter sample and a determined working condition to form a model prior sample set; s3, according to the model prior sample set, constructing a flow field wall
surface pressure prediction model under
shock wave boundary layer interference based on an improved Bayesian neural network; and S4, based on the flow field wall
surface pressure prediction model under the interference of the
shock wave boundary layer, performing adaptive parameter identification on the SST turbulence model by adopting a
particle swarm optimization algorithm to obtain the optimal closing parameter of the SST turbulence model for realizing the high-precision
simulation of the flow field. According to the method, the numerical
simulation precision and speed are improved, and
technical support is provided for safe and reliable work of the
scramjet engine in a complex environment.