some results
TRANSCRIPT
Investigation of Transition Scenario over an Airfoil using Direct Numerical Simulation
Top: Transition scenarios over an airfoil, Middle: Transition scenarios on flat-plate, and Bottom: shock/shear layer interaction.
X
Y
Z
0.03500.03110.02720.02330.01940.01560.01170.00780.00390.0000
t=9T
t=8T
t=4T
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
t=2T
Investigation of Transition Scenario over an Airfoil using Direct Numerical Simulation
Top: Transition scenarios over an airfoil, Middle: Transition scenarios on flat-plate, and Bottom: shock/shear layer interaction.
X
Y
Z
0.03500.03110.02720.02330.01940.01560.01170.00780.00390.0000
t=9T
t=8T
t=4T
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1
t=2T
t=8T
t=4T
t=2T
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
t=T
Investigation of Transition Scenario over an Airfoil using Direct Numerical Simulation
Top: Transition scenarios over an airfoil, Middle: Transition scenarios on flat-plate, and Bottom: shock/shear layer interaction.
t=8T
t=4T
t=2T
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9
t=T