kynema_sgf::actuator::FlatPlateData Struct Reference

#include <FlatPlate.H>

Inheritance diagram for kynema_sgf::actuator::FlatPlateData:

Collaboration diagram for kynema_sgf::actuator::FlatPlateData:

Public Attributes
amrex::Real	chord_inp {1.0_rt}
amrex::Real	cd_factor {0.0_rt}
ThinAirfoil	aflookup
Public Attributes inherited from kynema_sgf::actuator::WingBaseData
int	num_pts
	Number of points along the wing.
vs::Vector	start
	Starting coordinate of the wing.
vs::Vector	end
	Ending coordinate of the wing.
vs::Vector	blade_x {1.0_rt, 0, 0}
	The normal vector perpendicular to the span.
vs::Vector	eps_inp
	Gaussian smearing factor input by user.
vs::Vector	epsilon_chord
	epsilon / chord
amrex::Real	pitch {0.0_rt}
	Pitch angle for the wing.
bool	gauss_2D {false}
	Switch for turning on 2D Gaussian (off in spanwise)
bool	normalize_2D_spanwise {true}
	Switch for spanwise normalization in 2D setting.
amrex::Vector< int >	force_coord_flags {1, 1, 1}
	Switch for turning off force components of actuator.
amrex::Real	prescribed_uinf {-1.0_rt}
	User-specified velocity magnitude, only active when nonnegative.
std::string	pitch_timetable_file
	File name for pitch actuation table.
amrex::Vector< amrex::Real >	time_table
	Pitch actuation: time table.
amrex::Vector< amrex::Real >	pitch_table
	Pitch actuation: pitch angle table.
VecList	vel_rel
	Relative velocity at the actuator node.
vs::Vector	vel_tr {0.0_rt, 0.0_rt, 0.0_rt}
	Translational velocity.
std::string	motion_type {"none"}
	Wing motion type.
vs::Vector	s_vector {0.0_rt, 0.0_rt, 0.0_rt}
	Parameters for sine motions.
amrex::Real	s_period {0.0_rt}
std::unique_ptr< FLLCData >	fllc
	Filtered Lifting Line Correction data.
ComponentView	component_view
	Data structure required for passing data to the FLLC.
RealList	dx
	Width of actuator sections.
RealList	aoa
	Angle of attack at actuator nodes.
RealList	cl
	Computed lift coefficient at actuator nodes.
RealList	cd
	Computed drag coefficient at actuator nodes.
RealList	chord
	Chord length at the actuator nodes.
amrex::Real	lift {0.0_rt}
	Total integrated lift over the wing.
amrex::Real	drag {0.0_rt}
	Total integrated drag over the wing.

Member Data Documentation

aflookup

ThinAirfoil kynema_sgf::actuator::FlatPlateData::aflookup

cd_factor

amrex::Real kynema_sgf::actuator::FlatPlateData::cd_factor {0.0_rt}

chord_inp

amrex::Real kynema_sgf::actuator::FlatPlateData::chord_inp {1.0_rt}

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The documentation for this struct was generated from the following file:

• /home/runner/work/kynema-sgf/kynema-sgf/src/wind_energy/actuator/wing/FlatPlate.H