The deviation between the model and experimental data is not more than 10% in turbulent flow zone and 19% in non-turbulent flow zone. 该模型经实验验证,在非湍流区偏差不超过10%,在全湍流区偏差不超过19%。
Based on the liner stability analysis, a approach that treats non-turbulent fluctuations in a turbulence-like manner is used to research supersonic flow transition including onset and extent of transition. 基于线性稳定性的结果,以类似于处理湍流脉动的方式来模化流场脉动,用以研究高超声速的流动转捩,包括转捩起始位置及转捩区长度。