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Present results of all grid resolutions and then plot the results of the fine-level grid separately. If you want to see other results of the gird level, you can see them at "vandv_files/LMmodel".
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All of the flat plate results(= attached flow) are in good agreement with the Fluent results. But, the Airfoil results have the oscillation near the separation region both Fluent and SU2.
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### T3A
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The experiment data from [here](http://cfd.mace.manchester.ac.uk/ercoftac/)
@@ -102,13 +113,25 @@ Mesh_6 : Ultra Fine
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### NLF0416
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Fluent and SU2, the NLF-0416 airfoil results oscillate near the separation region. So, Here are shown only the fine-level grid results of every 1000 iterations and the instantaneous.
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C : Coarse
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M : Medium
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F : Fine
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X : Extra fine
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Every 1000 iteration results :
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<palign="center">
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<imgsrc="/vandv_files/LM_model/NLF/Delta_1000_Fine_Cp.png"alt="Fine level result comparsion of Cp distribution on NLF-0416" />
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<imgsrc="/vandv_files/LM_model/NLF/Delta_1000_Fine_Cf.png"alt="Fine level result comparsion of Cf distribution on NLF-0416" />
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Instantaneous result is :
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<palign="center">
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<imgsrc="/vandv_files/LM_model/NLF/Inst_All_Cp.png"alt="Fine level result comparsion of Cp distribution on NLF-0416" />
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<imgsrc="/vandv_files/LM_model/NLF/Inst_All_Cf.png"alt="Fine level result comparsion of Cf distribution on NLF-0416" />
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<imgsrc="/vandv_files/LM_model/NLF/Inst_Fine_Cp.png"alt="Fine level result comparsion of Cp distribution on NLF-0416" />
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<imgsrc="/vandv_files/LM_model/NLF/Inst_Fine_Cf.png"alt="Fine level result comparsion of Cf distribution on NLF-0416" />
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