The purpose of this paper is to introduce a unique technique to couple the two-integral boundary layer solutions to a generic inviscid solver in an iterative fashion.
Reference:
Smith, L, Oxtoby, O, Malan, A and Meyer, J. 2013. An interactive boundary layer modelling methodology for aerodynamic flows. International Journal of Numerical Methods for Heat & Fluid Flow, vol. 23(8), pp 1373-1392
Smith, L., Oxtoby, O. F., Malan, A., & Meyer, J. (2013). An interactive boundary layer modelling methodology for aerodynamic flows. http://hdl.handle.net/10204/7163
Smith, L, Oliver F Oxtoby, A Malan, and J Meyer "An interactive boundary layer modelling methodology for aerodynamic flows." (2013) http://hdl.handle.net/10204/7163
Smith L, Oxtoby OF, Malan A, Meyer J. An interactive boundary layer modelling methodology for aerodynamic flows. 2013; http://hdl.handle.net/10204/7163.
Copyright: 2013 Emerald. This is the pre/post print version of the work. The definitive version is published in International Journal of Numerical Methods for Heat & Fluid Flow, vol. 23(8), pp 1373-1392
