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Forum: FLUENT

May 7, 2010, 16:17

Replies: 28

transition point

Views: 8,737

Posted By galtmann

2003-3516 "Active Separation Control -...

2003-3516 "Active Separation Control - Measurements and Computations
for a NACA 0036 Airfoil"
2006-322 "Control of Massive Separation on A Thick-Airfoil Wing: A Computational and Experimental...

Forum: FLUENT

May 7, 2010, 13:04

Replies: 28

transition point

Views: 8,737

Posted By galtmann

Mach: 0.07 Re: 1.08x10^6 Alpha: for this...

Mach: 0.07
Re: 1.08x10^6
Alpha: for this case, 0 degrees
Airfoil: NACA0036 to simulate bluff bodies
Turbulence Model: Both k-w SST, and Transition SST found in Fluent 12.1
y+: all less than 1...

Forum: FLUENT

May 7, 2010, 02:02

Replies: 28

transition point

Views: 8,737

Posted By galtmann

Yea... I just tried running a laminar zone before...

Yea... I just tried running a laminar zone before the trip strip, and then turbulent everywhere else and I did not match my experimental data; the solution was the same as the baseline case where the...

Forum: FLUENT

May 3, 2010, 18:34

Replies: 28

transition point

Views: 8,737

Posted By galtmann

I'm trying to model forced transition with a trip...

I'm trying to model forced transition with a trip strip on a 2D airfoil in fluent 12.1. I did not think about trying to split the entire domain into two zones, so I'll try that, but the original way...

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