------- BEAMDYN Driver with OpenFAST INPUT FILE --------------------------------
Static analysis of NREL 5MW blade under distributed force
---------------------- SIMULATION CONTROL --------------------------------------
False DynamicSolve - Dynamic solve (false for static solve) (-)
0 t_initial - Starting time of simulation (s) [used only when DynamicSolve=TRUE]
30 t_final - Ending time of simulation (s) [used only when DynamicSolve=TRUE]
0.002 dt - Time increment size (s) [used only when DynamicSolve=TRUE]
---------------------- GRAVITY PARAMETER --------------------------------------
0 Gx - Component of gravity vector along X direction (m/s^2)
0 Gy - Component of gravity vector along Y direction (m/s^2)
0 Gz - Component of gravity vector along Z direction (m/s^2)
---------------------- FRAME PARAMETER --------------------------------------
0 GlbPos(1) - Component of position vector of the reference blade frame along X direction (m)
0 GlbPos(2) - Component of position vector of the reference blade frame along Y direction (m)
1 GlbPos(3) - Component of position vector of the reference blade frame along Z direction (m)
---The following 3 by 3 matrix is the direction cosine matirx ,GlbDCM(3,3),
---relates global frame to the initial blade root frame
1.0000000E+00 0.0000000E+00 0.0000000E+00
0.0000000E+00 1.0000000E+00 0.0000000E+00
0.0000000E+00 0.0000000E+00 1.0000000E+00
True GlbRotBladeT0 - Reference orientation for BeamDyn calculations is aligned with initial blade root?
---------------------- ROOT VELOCITY PARAMETER ----------------------------------
0 RootVel(4) - Component of angular velocity vector of the beam root about X axis (rad/s)
0 RootVel(5) - Component of angular velocity vector of the beam root about Y axis (rad/s)
0 RootVel(6) - Component of angular velocity vector of the beam root about Z axis (rad/s)
---------------------- APPLIED FORCE ----------------------------------
10000 DistrLoad(1) - Component of distributed force vector along X direction (N/m)
0 DistrLoad(2) - Component of distributed force vector along Y direction (N/m)
0 DistrLoad(3) - Component of distributed force vector along Z direction (N/m)
0 DistrLoad(4) - Component of distributed moment vector along X direction (N-m/m)
0 DistrLoad(5) - Component of distributed moment vector along Y direction (N-m/m)
0 DistrLoad(6) - Component of distributed moment vector along Z direction (N-m/m)
0 TipLoad(1) - Component of concentrated force vector at blade tip along X direction (N)
0 TipLoad(2) - Component of concentrated force vector at blade tip along Y direction (N)
0 TipLoad(3) - Component of concentrated force vector at blade tip along Z direction (N)
0 TipLoad(4) - Component of concentrated moment vector at blade tip along X direction (N-m)
0 TipLoad(5) - Component of concentrated moment vector at blade tip along Y direction (N-m)
0 TipLoad(6) - Component of concentrated moment vector at blade tip along Z direction (N-m)
0 NumPointLoads - Number of point loads along blade
Non-dim blade-span eta Fx Fy Fz Mx My Mz
(-) (N) (N) (N) (N-m) (N-m) (N-m)
---------------------- PRIMARY INPUT FILE --------------------------------------
"bd_primary_nrel_5mw.inp" InputFile - Name of the primary BeamDyn input file