Stall Mitigation and Lift Enhancement of NACA 0012 with Triangle-Shaped Surface Protrusion at a Reynolds Number of 105
Transient numerical simulations are conducted over a NACA 0012 airfoil with triangular
protrusions at a Reynolds number (Re) of 100000 using the γ-Reθ transition Shear Stress …
protrusions at a Reynolds number (Re) of 100000 using the γ-Reθ transition Shear Stress …
Investigation of effects of sand particles on aerodynamic performance of NACA 0012 airfoil
F Kaya - Niğde Ömer Halisdemir Üniversitesi Mühendislik …, 2023 - dergipark.org.tr
Öz The purpose of this paper is to study the effects of turbulence kinetic energy structures
formed during flow and particles of different diameters and different flow velocities in the air …
formed during flow and particles of different diameters and different flow velocities in the air …
[PDF][PDF] Investigation of effects of sand particles on aerodynamic performance of NACA 0012 airfoil NACA 0012 kanat profilinin aerodinamik performansı üzerinde toz …
F Kaya - scholar.archive.org
Öz The purpose of this paper is to study the effects of turbulence kinetic energy structures
formed during flow and particles of different diameters and different flow velocities in the air …
formed during flow and particles of different diameters and different flow velocities in the air …