Closed maucollu closed 4 months ago
Hello, Figure 6 here https://onlinelibrary.wiley.com/doi/pdf/10.1002/we.2703 suggests a value closer to 0.5 than 1.0
Thanks a lot, @ptrbortolotti for the quick answer. Interesting study, indeed, the value seems to be lower than 1.0. I also noticed, though, that it states "Fortunately, most large downwind turbine will have large Reynolds numbers in the supercritical range, as shown by that for the SUMR-13, so that C_D = 0.7 is a good approximation". As far as I know, 0.7 is indeed the value at which it stabilises in post-critical regime, and some handbooks/recommended practices recommend to round it up to 1.0 as safety factor. Would you think that a value of 0.7 is more appropriate, based on the statement above?
Description
It is not so much as a bug, but a doubt about the value of the parametrt
TwrCd
in the Aerodyn15.dat file of the IEA15MW UMaine Semisub, section "Tower Influence and Aerodynamics".The value is
0.5
for all the sections.I suppose that the drag, evaluated quasi statically with a simple drag equation such as: D = 1/2 x air density x (relative wind velocity)^2 x reference area * C_d
where the reference area is the diameter of the tower multiplied by the height of the section of the tower considered.
If the above is correct, for a circular section, in post-critical regime, the C_d should be 1.0 (see, for example, DNV-RP-C205 (Sept 2021), Appendix E. Table E-1, geometry 14.
Have I misunderstood something?
Steps to reproduce issue
Please provide a minimum working example (MWE) if possible N.A.
Current behavior
TwrCd 0.5
in AeroDyn15.datExpected behavior
TwrCd 1.0
in AeroDyn15.datCode versions
N.A.