We introduce an open-source and unified framework for transition analysis for laminar boundary layer natural transition at transonic conditions and over complex geometries, where surface irregularities may be present. Different computational tools are integrated in the framework, and therefore overcomes the difficulties of two separate and usually quite disparate processes when using $e^N$ method for transition analysis. To generate a baseflow with desired pressure distribution, appropriate pressure compatible inflow boundary condition needs to be developed and enforced. We first derive the system for 1D numerical stability analysis for boundary conditions, and construct three types of pressure compatible inflow. We demonstrate that the entropy-pressure compatible inflow is stable unlike other choices. Compared with the steady baseflow computation, the unsteady simulation for the disturbance field is more challenging for compressible flows because of complex wave reflections, which can easily contaminate the results. We therefore introduce the two main sources of wave decontamination and corresponding methods to obtain clean signal. The workflow within the framework is then verified by computing the disturbance development in 2D flat plate boundary layer flows at Mach $0.8$. The $N$-factors over a clean flat plate and a flat plate with a forward-facing step are generated, and agree well with the results from the reference. Following the verified workflow, We then analyze the disturbance growth on a wing section of the CRM-NLF model. The N-factor on a 2D simulation is generated and studied.
翻译:我们引入了一个开放源码和统一框架,用于在跨音质条件下和复杂地貌上进行Laminar边界层自然过渡的过渡分析,其中可能存在表面异常现象。不同的计算工具被纳入框架,从而克服了在使用美元转换分析方法时两个单独和通常相当不同的过程的困难。为了产生一个有理想的压力分布的基流,需要开发和实施适当的压力兼容的流入边界条件。我们首先为边界条件得出1D数字稳定分析系统,并建造三种压力兼容的流入。我们证明,与其它选择不同的是,通气压流入稳定。与稳定的基流计算相比,由于复杂的波反射反射,扰动场的不稳模拟对可压缩的流量更具挑战性,这很容易污染结果。因此,我们引入了两种主要的波净化源和相应的获取清洁信号的方法。随后通过计算2D平面板板底板边界层的扰动动态,以Mach 0. 0. 80美元计算出三层的扰动发展动态。在清洁平板板的基流上,以美元计算出一个平板和后方平面的平面分析结果。