作者: S. R. Batenko , V. I. Terekhov
关键词:
摘要: The effect of dynamic prehistory the flow and channel‐expansion ratio on aerodynamics a steady separated laminar behind rectangular backward‐facing step located in plane‐parallel channel is numerically studied. It shown that boundary layer upstream separation exerts strong characteristics step. A decrease boundary‐layer thickness cross section leads to separation‐region length, an increase with fixed initial Reynolds number length.