We examine the structure of Direct Simulation Monte Carlo (DSMC)-resolved internal compression layers in rarefied micro-nozzle flows and show that their apparent parametric complexity is largely a registration and finite-thickness scaling effect. A density-gradient diagnostic identifies the compression-layer station , while a jump-based thickness defines a shock-centered coordinate . In physical coordinates, the leading proper orthogonal decomposition (POD) mode of the centerline density profiles captures only of the fluctuation energy, whereas the jump-scaled coordinate increases this value to . A two-dimensional shock-window POD further confirms that this compactness is not a centerline artifact: in the registered frame, the first density mode captures and the first two modes capture of the fluctuation energy. The same region is identified by density-gradient and gradient-length Knudsen-number diagnostics, linking the reduced representation to localized short-gradient-length rarefaction rather than to shock motion alone. We then use this structure as an inductive bias in a shock-aligned Fusion–Deep Operator Network (DeepONet) surrogate for density, velocity components, temperature, Mach number, and pressure. For held-out back-pressure cases, density, temperature, and pressure errors remain below , , and , respectively, and the hardest case reduces the shock-window mean error from – for standard baselines to . The results show that improved prediction follows from the reduced shock-centered structure of the DSMC fields rather than from network capacity alone.

生成讲解博客的中文版本

生成AI智能校验的中文版本