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Related to #30. This might also include the fact that one dataset from Sandia was used to optimize (?) the Sheldahl and Klimas static foil data for VAWTs. @wosnik probably understood this better than …
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From @johnpauls
1) This is from the Suitland Parkway which heads east out of Washington DC.
![image](https://cloud.githubusercontent.com/assets/5996979/8982912/a9a0f5a0-3693-11e5-8468-c92c87b772c1.pn…
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- [ ] some success in onshore wind, ultimatley failure
- [x] I know you like "clean" slides, but add locations of ORPC installations
- [ ] maybe a schematic that explains "one-geometric-parameter" (D…
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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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```
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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The aircraft (at least the base wheels variant) cruises with significant nose-down attitude. Even in climb at 120 knots it already flies with alpha = -2.50 and at a 140 knot cruise it flies with alpha…
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This tutorial simulates the UNH-RVAT, which should hit a mean power coefficient of roughly 25%.
The `C_P` waveform looks the most accurate of all the DS models, but the amplitude and mean values are…
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The simulation of inviscid supersonic air flowing over flat plate was tested. It ran on multi-CPUs(MPI)
It was always failed, and I could not find out any problems.
The flow parameters were as below:…
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There are convergence issues at high angle of attack that may require unsteady simulations?
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Based on the number of points, I believe what is currently labeled the 449 x 129 mesh is actually the 225 x 65, and what is labeled the 897 x 257 mesh is actually the 449 x 129