@inproceedings{2b8052dca213453a8fbf23c45c131304,
title = "Validation of numerical simulation method for active flow control technology",
abstract = "The numerical simulation method of active flow control technology was studied in this paper. The simplified mathematical model of the active flow control is established with unsteady velocity boundary condition at the specific location of model surface. The reliability of flow control model was verified by standard cases of CFDVAL2004, and the capability of capturing micro-jet flow characteristics for Spalart-Allmaras (SA) and Menter's Shear Stress Transport (SST) turbulence model were analyzed. The results showed that the accuracy of SA turbulence model is better than the SST model, and flow control model meet the accuracy requirements for numerical simulation method.",
keywords = "Active flow control, Numerical simulation, Synthetic jet, Unsteady",
author = "Xu, \{Xiao Ping\} and Zhou Zhou",
year = "2014",
doi = "10.4028/www.scientific.net/AMR.1016.694",
language = "英语",
isbn = "9783038352235",
series = "Advanced Materials Research",
publisher = "Trans Tech Publications Ltd",
pages = "694--699",
booktitle = "Mechanical and Aerospace Engineering V",
note = "5th International Conference on Mechanical and Aerospace Engineering, ICMAE 2014 ; Conference date: 18-07-2014 Through 19-07-2014",
}