Dear all,
According to the AeroDyn.dat file in OpenFAST v4.1.2, the software can output aerodynamic loads for a maximum of 9 nodes (NTwOuts <= 9). Taking the IEA-15MW-UMaine floating wind turbine as an example, the tower discretization in the AeroDyn.dat file is defined as follows:
TwrElev TwrDiam TwrCd TwrTI TwrCb
(m) (m) (-) (-) (-)
15. 10. 0.5 0.1 0.0
28. 10. 0.5 0.1 0.0
41. 10. 0.5 0.1 0.0
54. 10. 0.5 0.1 0.0
67. 10. 0.5 0.1 0.0
80. 10. 0.5 0.1 0.0
93. 10. 0.5 0.1 0.0
106. 10. 0.5 0.1 0.0
119. 10. 0.5 0.1 0.0
132. 10. 0.5 0.1 0.0
144.386 6.5 0.5 0.1 0.0
There are eleven nodes in total, dividing the tower into 10 segments. However, because the maximum value for NTwOuts is capped at 9, the aerodynamic loads across all 11 nodes cannot be displayed simultaneously.
If the output is indeed strictly limited to 9 nodes, does Node 1 correspond to the point at TwrElev = 15 (which should represent the tower base), Node 2 correspond to TwrElev = 28, and so on, up to Node 9 corresponding to TwrElev = 119?
If this assumption is correct, and I request the output variable 'TwN1Fdx' (the x-component of the aerodynamic drag force per unit length at tower node 1), what is the appropriate tributary length I should multiply TwN1Fdx by to obtain the total integrated x-component drag force for the segment corresponding to Tower Node 1?
Thank you in advance for your help!
Dear all,
According to the AeroDyn.dat file in OpenFAST v4.1.2, the software can output aerodynamic loads for a maximum of 9 nodes (NTwOuts <= 9). Taking the IEA-15MW-UMaine floating wind turbine as an example, the tower discretization in the AeroDyn.dat file is defined as follows:
TwrElev TwrDiam TwrCd TwrTI TwrCb
(m) (m) (-) (-) (-)
15. 10. 0.5 0.1 0.0
28. 10. 0.5 0.1 0.0
41. 10. 0.5 0.1 0.0
54. 10. 0.5 0.1 0.0
67. 10. 0.5 0.1 0.0
80. 10. 0.5 0.1 0.0
93. 10. 0.5 0.1 0.0
106. 10. 0.5 0.1 0.0
119. 10. 0.5 0.1 0.0
132. 10. 0.5 0.1 0.0
144.386 6.5 0.5 0.1 0.0
There are eleven nodes in total, dividing the tower into 10 segments. However, because the maximum value for NTwOuts is capped at 9, the aerodynamic loads across all 11 nodes cannot be displayed simultaneously.
If the output is indeed strictly limited to 9 nodes, does Node 1 correspond to the point at TwrElev = 15 (which should represent the tower base), Node 2 correspond to TwrElev = 28, and so on, up to Node 9 corresponding to TwrElev = 119?
If this assumption is correct, and I request the output variable 'TwN1Fdx' (the x-component of the aerodynamic drag force per unit length at tower node 1), what is the appropriate tributary length I should multiply TwN1Fdx by to obtain the total integrated x-component drag force for the segment corresponding to Tower Node 1?
Thank you in advance for your help!