Mehmet Sarimurat

Research interests: Shock location management, supersonic compressors, supersonic inlets, shock boundary layer interaction, boundary layer control, compressible flow with flow blowing and suction, compressor aerodynamics

Publications:

1.       M. N. Sarimurat and T. Q. Dang “An Analytical Model for Boundary Layer Control via Steady Blowing and its Application to NACA-65-410 Cascade”, ASME Journal of Turbomachinery, Vol. 136, No. 6 (2014): 061011, doi: 10.1115/1.4025585 (pdf)

2.       M. N. Sarimurat and T. Q. Dang “Shock Management in Diverging Flow Passages by Blowing/Suction Part 1: Quasi-1D Theory”, AIAA Journal of Propulsion and Power, Vol. 28, Issue 6, 2012, pp. 1222-1229, doi: 10.2514/1.B34136 (pdf)

3.       M. N. Sarimurat and T. Q. Dang “Shock Management in Diverging Flow Passages by Blowing/Suction Part 2: Applications”, AIAA Journal of Propulsion and Power, Vol. 28, Issue 6, 2012, pp.1230-1242, doi: 10.2514/1.B34137 (pdf)