Numerical Simulation of Backward Step and Jet Exhaust Flows

摘要

Preparatory to a continuing study of efficient, high resolution flow structure capture on patched mesh systems, turbulent flowfield solutions for a tactical missile base flow problem are computed on two first level composite grids of differing topologies. One mesh is of the wraparound character and the other is a step mesh on the cartesian topology. A simplified Baldwin-Lomax algebraic eddy viscosity model is applied in the wake region. Results for the two meshes are compared with each other and with other computations reported in the literature. The totality of results suggest both mesh topology and resolution are important factors in the accuracy of predictive results as well as turbulence modeling. Related to interests in high altitude laminar flows about bluff bodies such as the AOTV, this reprint also presents results from a solution for laminar flow over a backward facing step and makes comparison with the available classical experiment of Chapman, et al. Keywords: Navier Stokes equations; Computations. (Author)