Closed pelljam closed 2 weeks ago
Hello James, this is a great catch. It took me a bit of digging to understand why Cd0 is set to 0. I found that back in 2021 I zeroed out this term during a V&V study because things weren't matching, and zeroing Cd0 helped greatly. This happened in WISDEM commit https://github.com/WISDEM/WISDEM/commit/4271c970f13abeef4bd4e82d1c603c7335c915a6 However we now know that we were plagued by multiple other issues in OpenFAST, and so that zeroing of Cd0 might have simply be a lucky coincidence. I will try to turn it back on and see what happens. It will take me a few days to run all the checks, but it's high among my todos
I've pushed new airfoil files here https://github.com/IEAWindTask37/IEA-22-280-RWT/tree/openfast_fixes I'm running some tests to make sure they perform as expected
Hello again, Once merged, this PR https://github.com/IEAWindTask37/IEA-22-280-RWT/pull/75 will fix the issue of Cd0. Note however that I haven't seen much effect (almost anything) in the time-domain turbulent-wind results. I have not processed the linearized-domain results yet. However generating a good Campbell by linearizing the OpenFAST with unsteady aero airfoil turned on is a little time consuming at the moment, so this will take me a while
Thanks Pietro. For what it's worth, I observed a noticeable difference between OrcaFlex and OpenFAST, in some time-domain results, which I can attribute to this data (because once I set Cd0 for all airfoils in OrcaFlex, the results converged). Although off the top of my head, I can't remember the details. I can have a closer look, if you are interested? Which UA model are you running? My investigation uses the González model, possibly that choice will dictate the sensitivity to this data?
I've been toggling between UAMod 3, which works better with ElastoDyn (@dzalkind can confirm), and UAMod 4, which works better for BeamDyn. We suspect that there is a dependency to the time step size, which must be very small with BeamDyn (we are close to fixing that). The two models are different implementations of the Beddoes-Leishman unsteady aero model https://openfast.readthedocs.io/en/main/source/user/aerodyn/theory_ua.html#beddoes-leishman-4-states-model-uamod-4
Hi,
I just wondered if it was intentional that Cd0 (2D drag coefficient value at 0-lift) is zero for all airfoils?
Thanks,
James