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OpenFAST
Wind turbine multiphysics simulator
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OpenFAST
Wind turbine multiphysics simulator
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Public Attributes | |
| 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 | cp |
| 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 | vind_cp |
| Induced velocity on lifting line control points [m/s]. | |
| real(reki), dimension(:,:), allocatable | vtot_cp |
| Total velocity on lifting line control points [m/s]. | |
| real(reki), dimension(:,:), allocatable | vstr_cp |
| Structural velocity on LL CP [m/s]. | |
| real(reki), dimension(:,:), allocatable | vwnd_cp |
| 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]. | |
| real(reki), dimension(:), allocatable | pitchandtwist |
| Twist angle (includes all sources of twist) [Array of size (NumBlNds,numBlades)] [rad]. | |
| integer(intki) | itip |
| Index where tip vorticity will be placed. More... | |
| integer(intki) | iroot |
| Index where root vorticity will be placed [-]. | |
| 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 [-]. | |
| type(ua_inputtype), dimension(:,:), allocatable | u_ua |
| inputs to UnsteadyAero numNode x 2 (t and t+dt) [-] | |
| 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 [-] | |
| real(reki), dimension(:,:), allocatable | vind_ll |
| Induced velocity on lifting line nodes [m/s]. | |
| 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_cpmin |
| Coefficient minimum pressure, 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 [-] | |
| real(reki), dimension(:), allocatable fvw_types::wng_miscvartype::bn_cd_static |
Coefficient drag.
excluding unsteady aero effects [-]
| integer(intki) fvw_types::wng_miscvartype::itip |
Index where tip vorticity will be placed.
TODO, per blade [-]
1.8.13