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Default Cases Transition Modeling - Geometries and Experimental Results

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Old   August 5, 2019, 20:45
Question Default Cases Transition Modeling - Geometries and Experimental Results
Join Date: Apr 2012
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leo_NM is on a distinguished road
Good Night.

I am a Ph.D student currently trying to join a few cases to test some transition modeling implementation.

What I usually see as common transition models test cases are:

- ERCOFTAC T3 flat plates.
- 30p30n Multi-Element Airfoil
- Aerospatiale-A airfoil.
- S809 Airfoil (wind-Turbine)
- NASA NLF(1)-0416 airfoil.
- Inclined, 6:1 Prolate Spheroid (*)

- TU Braunschweig Sickle Wing (*)

- DLR-F5 wing
- DLR-F4 Wing body
- MBB VA-2 Airfoil (*)


The cases highlighted with (*) are the cases which the geometric/experimental definition are not readily available in the internet. Unfortunately, these cases would be the most interesting ones for my theses as crossflow transition is the main mechanism on these geometries. My question is:

How can I get access to these geometries and experimental results. Is there any other case repository which is not documented in the NASA TMR website ?

A nice reference which I used to build the list is:

AIAA 2018-0029

Thank You !!
leo_NM is offline   Reply With Quote


crossflow, rans, transition

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