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From Cynthia @ NCR, 12/22/15:
> I've attached a boundary feature class that covers all of NCR. I'm not confident that I have the right boundary data for CHOH and GWMP. What I compiled is based on L…
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DATCOM needs a designation as to which NACA Airfoil designation belongs to
which wing. This designation is done in the following format as an example:
NACA-W-6-66-012
NACA-H-6-66-009
NACA-V-6-66…
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There will need to be a measure of the distance from the end to each `actuatorLineElement`.
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Chamorro et al. (2012) showed that an AFT wake became Re-independent at `Re_D ~ 10^5`. I haven't see much about the performance of AFTs though. I know that a low-Re model will need a different blade, …
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The NACA 0012 Mesh (mesh_NACA0012_turb_897x257.su2) does not match the input file format. It is listed as a 2-dimensional mesh, but there are three floating point numbers and then a node number.
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As several people noticed, the 160 hp-powered c172p is under-powered, which makes it "lazy" at full load. Floats and amphibious worsen everything (added drag).
I tried to fiddle the propeller pitch an…
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The SU2 mesh file format states that elements must have node numbers ("The final value is the element index given to each interior element in the mesh"). The NACA 0012 mesh does not have them, and thu…
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md01x から md02x への見直しで High Downforce 仕様でもバランス的におかしくないようにしたつもりだけど... 未だに腑に落ちていないのが Rear Wing の感じ.
![fp-021_rr-wing_cap01](https://cloud.githubusercontent.com/assets/3119480/8506011/5b3b6a3a-2239-11e5-…
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The NACA 0012 test case (TestCases/rans/naca0012) does not converge with the provided config file if RESTART_SOL=NO, and the number of iterations is increased beyond 25. The test case should be update…
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As in Dyachuk et al. (2014). Should derive from `LeishmanBeddoes`.