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OpenFAST
Wind turbine multiphysics simulator
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Public Attributes | |
logical | firstcall |
True if this is the first call to update state (used in CalcOutput) [-]. | |
real(reki), dimension(:,:,:), allocatable | le |
Leading edge points [-]. | |
real(reki), dimension(:,:,:), allocatable | te |
Trailing edge points [-]. | |
real(reki), dimension(:,:,:,:), allocatable | r_ll |
Position of the Lifting line panels [-]. | |
real(reki), dimension(:,:), allocatable | s_ll |
Spanwise coordinate of LL elements [m]. | |
real(reki), dimension(:,:), allocatable | chord_ll |
chord on LL nodes [m] | |
real(reki), dimension(:,:), allocatable | s_cp_ll |
Spanwise coordinate of LL CP [m]. | |
real(reki), dimension(:,:), allocatable | chord_cp_ll |
chord on LL cp [m] | |
real(reki), dimension(:,:,:), allocatable | cp_ll |
Coordinates of LL CP [-]. | |
real(reki), dimension(:,:,:), allocatable | tang |
Unit Tangential vector on LL CP [-]. | |
real(reki), dimension(:,:,:), allocatable | norm |
Unit Normal vector on LL CP [-]. | |
real(reki), dimension(:,:,:), allocatable | orth |
Unit Orthogonal vector on LL CP [-]. | |
real(reki), dimension(:,:,:), allocatable | dl |
Vector of elementary length along the LL [-]. | |
real(reki), dimension(:,:), allocatable | area |
Area of each LL panel [-]. | |
real(reki), dimension(:,:), allocatable | diag_ll |
Diagonal length of each LL panel [-]. | |
real(reki), dimension(:,:), allocatable | gamma_ll |
Circulation on the wing lifting line (COPY of Constraint State) [-]. | |
real(reki), dimension(:,:,:), allocatable | vind_ll |
Induced velocity on lifting line control points [m/s]. | |
real(reki), dimension(:,:,:), allocatable | vtot_ll |
Total velocity on lifting line control points [m/s]. | |
real(reki), dimension(:,:,:), allocatable | vstr_ll |
Structural velocity on LL CP [m/s]. | |
real(reki), dimension(:,:,:), allocatable | vwnd_ll |
Wind on lifting line control points [m/s]. | |
real(reki), dimension(:,:,:,:), allocatable | vwnd_nw |
Wind on near wake panels [m/s]. | |
real(reki), dimension(:,:,:,:), allocatable | vwnd_fw |
Wind on far wake panels [m/s]. | |
real(reki), dimension(:,:,:,:), allocatable | vind_nw |
Induced velocity on near wake panels [m/s]. | |
real(reki), dimension(:,:,:,:), allocatable | vind_fw |
Induced velocity on far wake panels [m/s]. | |
integer(intki) | nnw |
Number of active near wake panels [-]. | |
integer(intki) | nfw |
Number of active far wake panels [-]. | |
integer(intki) | istep |
Current step number used for update state [-]. | |
integer(intki) | vtkstep |
Current vtk output step number [-]. | |
real(dbki) | vtklasttime |
Time the last VTK file set was written out [s]. | |
real(reki), dimension(:,:), allocatable | r_wind |
List of points where wind is requested for next time step [-]. | |
real(reki), dimension(:,:), allocatable | pitchandtwist |
Twist angle (includes all sources of twist) [Array of size (NumBlNds,numBlades)] [rad]. | |
logical | computewakeinduced |
Compute induced velocities on this timestep [-]. | |
real(dbki) | oldwaketime |
Time the wake induction velocities were last calculated [s]. | |
real(reki) | tspent |
Time spent in expensive Biot-Savart computation [s]. | |
real(reki), dimension(:,:,:,:), allocatable | dxdt_nw |
State time derivatie, stored for subcylcing [-]. | |
real(reki), dimension(:,:,:,:), allocatable | dxdt_fw |
State time derivatie, stored for subcylcing [-]. | |
real(reki), dimension(:,:), allocatable | alpha_ll |
Angle of attack at lifting line CP, only computed with CircPolarData method [-]. | |
real(reki), dimension(:,:), allocatable | vreln_ll |
Norm of Vrel on the lifting line [-]. | |
integer(intki), dimension(:,:), allocatable | segconnct |
Connectivity of segments [-]. | |
real(reki), dimension(:,:), allocatable | segpoints |
Points delimiting the segments [-]. | |
real(reki), dimension(:), allocatable | seggamma |
Segment circulations [-]. | |
real(reki), dimension(:), allocatable | segepsilon |
Segment regularization parameter [-]. | |
real(reki), dimension(:,:), allocatable | cps |
Control points used for wake rollup computation [-]. | |
real(reki), dimension(:,:), allocatable | uind |
Induced velocities obtained at control points [-]. | |
real(reki), dimension(:,:), allocatable | bn_axind |
Axial induction [size: (NumBlNds,numBlades)] [-]. | |
real(reki), dimension(:,:), allocatable | bn_tanind |
Tangential induction [size: (NumBlNds,numBlades)] [-]. | |
real(reki), dimension(:,:), allocatable | bn_vrel |
Relative velocity [size: (NumBlNds,numBlades)] [m/s]. | |
real(reki), dimension(:,:), allocatable | bn_alpha |
Angle of attack [size: (NumBlNds,numBlades)] [rad]. | |
real(reki), dimension(:,:), allocatable | bn_phi |
angle between the plane of rotation and the direction of the local wind [size: (NumBlNds,numBlades)] [rad] | |
real(reki), dimension(:,:), allocatable | bn_re |
Reynolds number [size: (NumBlNds,numBlades)] [-]. | |
real(reki), dimension(:,:,:), allocatable | bn_urelwind_s |
Relative wind velocity in section coordinates [size: (3,NumBlNds,numBlades)] [m/s]. | |
real(reki), dimension(:,:), allocatable | bn_cl_static |
Coefficient lift, excluding unsteady aero effects [-]. | |
real(reki), dimension(:,:), allocatable | bn_cd_static |
Coefficient drag. More... | |
real(reki), dimension(:,:), allocatable | bn_cm_static |
Coefficient moment, excluding unsteady aero effects [-]. | |
real(reki), dimension(:,:), allocatable | bn_cl |
Coefficient lift, including unsteady aero effects [-]. | |
real(reki), dimension(:,:), allocatable | bn_cd |
Coefficient drag, including unsteady aero effects [-]. | |
real(reki), dimension(:,:), allocatable | bn_cm |
Coefficient moment, including unsteady aero effects [-]. | |
real(reki), dimension(:,:), allocatable | bn_cx |
normal force coefficient (normal to the plane, not chord) of the jth node in the kth blade [-] | |
real(reki), dimension(:,:), allocatable | bn_cy |
tangential force coefficient (tangential to the plane, not chord) of the jth node in the kth blade [-] | |
type(ua_miscvartype) | m_ua |
misc vars for UnsteadyAero [-] | |
type(ua_outputtype) | y_ua |
outputs from UnsteadyAero [-] | |
type(ua_parametertype) | p_ua |
parameters for UnsteadyAero [-] | |
logical | ua_flag |
logical flag indicating whether to use UnsteadyAero [-] | |
real(reki), dimension(:,:,:), allocatable | vwnd_nd |
InflowOnBlade (at nodes) values modified by tower influence. More... | |
real(reki), dimension(:,:), allocatable fvw_types::fvw_miscvartype::bn_cd_static |
Coefficient drag.
excluding unsteady aero effects [-]
real(reki), dimension(:,:,:), allocatable fvw_types::fvw_miscvartype::vwnd_nd |
InflowOnBlade (at nodes) values modified by tower influence.
ONLY for UA [m/s]