-
1
A CFD Assessment to Subsonic Flow Around NACA4412
Published 2011-12-01“…A 2-dimensional triangular C-type grid is used to match the reference measurements at an airfoil cross-section was taken from NACA 4412 from leading edge to trailing edge. …”
Get full text
Article -
2
Investigation of Leading Edge Film Cooling Jets in a Cross Flow
Published 2011-06-01“…Experimental and numerical simulations have been introduced to simulate a discrete circle hole film cooling flow over a symmetrical airfoil representing turbine guide vanes surface. …”
Get full text
Article