kynema::interfaces::components Namespace Reference

Classes
class	AerodynamicBody
struct	AerodynamicBodyInput
class	Aerodynamics
class	AerodynamicsBuilder
struct	AerodynamicSection
class	AerodynamicsInput
class	Beam
	Represents a turbine blade with nodes, elements, and constraints. More...
class	BeamBuilder
	Builder class for creating Blade objects. More...
struct	BeamInput
	Complete input specification for a beam. More...
struct	ControllerInput
	Configuration parameters for a DISCON-style turbine controller. More...
struct	Inflow
	Wind inflow model for turbine simulations. More...
struct	ReferenceAxis
	Reference axis definition for a beam. More...
struct	Root
	Root definition for a turbine beam. More...
struct	Section
	Sectional structural properties of the beam. More...
struct	SolutionBuilder
	A factory class for building a solution input, which is used by interfaces to control the time stepping proceedure. More...
struct	SolutionInput
	A configuration object used to create the low level StepParameters object. More...
class	Turbine
	Represents a turbine with nodes, elements, and constraints. More...
class	TurbineBuilder
	Builder class for creating Turbine objects with a fluent interface pattern. More...
struct	TurbineInput
	Complete input specification for a turbine. More...
struct	UniformFlow
	Uniform flow with time-dependent parameters. More...
struct	UniformFlowParameters
	Parameters defining uniform flow characteristics. More...

Enumerations
enum class	ReferenceAxisOrientation : std::uint8_t { X , Z }
	Enum to represent reference axis orientation. More...
enum class	InflowType : std::uint8_t { Uniform = 0 }
	Type of inflow model. More...

Functions
double	CalculateAngleOfAttack (std::span< const double, 3 > v_rel)
std::array< double, 6 >	CalculateAerodynamicLoad (std::span< double, 3 > ref_axis_moment, std::span< const double, 3 > v_inflow, std::span< const double, 3 > v_motion, std::span< const double > aoa_polar, std::span< const double > cl_polar, std::span< const double > cd_polar, std::span< const double > cm_polar, double chord, double delta_s, double fluid_density, std::span< const double, 3 > con_force, std::span< const double, 4 > qqr)
std::array< double, 3 >	CalculateConMotionVector (double ac_to_ref_axis_horizontal, double chord_to_ref_axis_vertical)
std::vector< double >	CalculateJacobianXi (std::span< const double > aero_node_xi)
std::vector< double >	CalculateAeroNodeWidths (std::span< const double > jacobian_xi, std::span< const double > jacobian_integration_matrix, std::span< const double > node_x)

Enumeration Type Documentation

InflowType

enum class kynema::interfaces::components::InflowType : std::uint8_t

strong

Type of inflow model.

Enumerator
Uniform	Uniform flow.

ReferenceAxisOrientation

enum class kynema::interfaces::components::ReferenceAxisOrientation : std::uint8_t

strong

Enum to represent reference axis orientation.

Enumerator
X
Z

Function Documentation

CalculateAerodynamicLoad()

std::array< double, 6 > kynema::interfaces::components::CalculateAerodynamicLoad	(	std::span< double, 3 >	ref_axis_moment,
		std::span< const double, 3 >	v_inflow,
		std::span< const double, 3 >	v_motion,
		std::span< const double >	aoa_polar,
		std::span< const double >	cl_polar,
		std::span< const double >	cd_polar,
		std::span< const double >	cm_polar,
		double	chord,
		double	delta_s,
		double	fluid_density,
		std::span< const double, 3 >	con_force,
		std::span< const double, 4 >	qqr
	)

CalculateAeroNodeWidths()

std::vector< double > kynema::interfaces::components::CalculateAeroNodeWidths	(	std::span< const double >	jacobian_xi,
		std::span< const double >	jacobian_integration_matrix,
		std::span< const double >	node_x
	)

CalculateAngleOfAttack()

double kynema::interfaces::components::CalculateAngleOfAttack

(

std::span< const double, 3 >

v_rel

)

CalculateConMotionVector()

std::array< double, 3 > kynema::interfaces::components::CalculateConMotionVector	(	double	ac_to_ref_axis_horizontal,
		double	chord_to_ref_axis_vertical
	)

CalculateJacobianXi()

std::vector< double > kynema::interfaces::components::CalculateJacobianXi

(

std::span< const double >

aero_node_xi

)