Numerical investigation of the low-frequency flow oscillation over a NACA-0012 aerofoil at the inception of stall
YA ElAwad, EM ElJack - International Journal of Micro Air …, 2019 - journals.sagepub.com
High-fidelity large eddy simulation is carried out for the flow field around a NACA-0012
aerofoil at Reynolds number of 9× 10 4, Mach number of 0.4, and various angles of attack …
aerofoil at Reynolds number of 9× 10 4, Mach number of 0.4, and various angles of attack …
Time Resolved Oscillating Behaviour of Laminar Separation Bubble Formed on an NACA-0012 Near Stall
GD Ramakrishna - AIAA SCITECH 2025 Forum, 2025 - arc.aiaa.org
Time-resolved particle image velocimetry (TR-PIV) is carried out for the flow field around a
NACA-0012 airfoil at a chord Reynolds number of = 1.9× 105, Mach number of 0.032 …
NACA-0012 airfoil at a chord Reynolds number of = 1.9× 105, Mach number of 0.032 …