kynema::interfaces::components::AerodynamicBody Class Reference

#include <aerodynamics.hpp>

Public Member Functions
	AerodynamicBody (const AerodynamicBodyInput &input, std::span< const Node > nodes)
template<typename DeviceType >
void	CalculateMotion (const HostState< DeviceType > &state)
void	SetInflowFromVector (std::span< const std::array< double, 3 > > inflow_velocity)
template<typename T >
void	SetInflowFromFunction (const T &inflow_velocity_function)
void	SetAerodynamicLoads (std::span< const std::array< double, 6 > > aerodynamic_loads)
void	CalculateAerodynamicLoads (double fluid_density)
void	CalculateNodalLoads ()
template<typename DeviceType >
void	AddNodalLoadsToState (HostState< DeviceType > &state)

Public Attributes
size_t	id
std::vector< size_t >	node_ids
std::vector< std::array< double, 7 > >	node_u
std::vector< std::array< double, 6 > >	node_v
std::vector< std::array< double, 6 > >	node_f
std::vector< std::array< double, 7 > >	xr_motion_map
std::vector< std::array< double, 7 > >	u_motion_map
std::vector< std::array< double, 6 > >	v_motion_map
std::vector< std::array< double, 4 > >	qqr_motion_map
std::vector< std::array< double, 3 > >	con_motion
std::vector< std::array< double, 3 > >	x_motion
std::vector< std::array< double, 3 > >	v_motion
std::vector< std::array< double, 3 > >	con_force
std::vector< std::array< double, 6 > >	loads
std::vector< std::array< double, 3 > >	ref_axis_moments
std::vector< double >	jacobian_xi
std::vector< std::array< double, 3 > >	v_inflow
std::vector< std::array< double, 3 > >	v_rel
std::vector< double >	twist
std::vector< double >	chord
std::vector< double >	delta_s
std::vector< size_t >	polar_size
std::vector< std::vector< double > >	aoa
std::vector< std::vector< double > >	cl
std::vector< std::vector< double > >	cd
std::vector< std::vector< double > >	cm
std::vector< double >	motion_interp
std::vector< double >	shape_deriv_jac

Constructor & Destructor Documentation

AerodynamicBody()

kynema::interfaces::components::AerodynamicBody::AerodynamicBody	(	const AerodynamicBodyInput &	input,
		std::span< const Node >	nodes
	)

Member Function Documentation

AddNodalLoadsToState()

template<typename DeviceType >

void kynema::interfaces::components::AerodynamicBody::AddNodalLoadsToState ( HostState< DeviceType > &  state )

inline

CalculateAerodynamicLoads()

void kynema::interfaces::components::AerodynamicBody::CalculateAerodynamicLoads

(

double

fluid_density

)

CalculateMotion()

template<typename DeviceType >

void kynema::interfaces::components::AerodynamicBody::CalculateMotion ( const HostState< DeviceType > &  state )

inline

CalculateNodalLoads()

void kynema::interfaces::components::AerodynamicBody::CalculateNodalLoads

(

)

SetAerodynamicLoads()

void kynema::interfaces::components::AerodynamicBody::SetAerodynamicLoads

(

std::span< const std::array< double, 6 > >

aerodynamic_loads

)

SetInflowFromFunction()

template<typename T >

void kynema::interfaces::components::AerodynamicBody::SetInflowFromFunction ( const T &  inflow_velocity_function )

inline

SetInflowFromVector()

void kynema::interfaces::components::AerodynamicBody::SetInflowFromVector

(

std::span< const std::array< double, 3 > >

inflow_velocity

)

Member Data Documentation

aoa

std::vector<std::vector<double> > kynema::interfaces::components::AerodynamicBody::aoa

cd

std::vector<std::vector<double> > kynema::interfaces::components::AerodynamicBody::cd

chord

std::vector<double> kynema::interfaces::components::AerodynamicBody::chord

cl

std::vector<std::vector<double> > kynema::interfaces::components::AerodynamicBody::cl

cm

std::vector<std::vector<double> > kynema::interfaces::components::AerodynamicBody::cm

con_force

std::vector<std::array<double, 3> > kynema::interfaces::components::AerodynamicBody::con_force

con_motion

std::vector<std::array<double, 3> > kynema::interfaces::components::AerodynamicBody::con_motion

delta_s

std::vector<double> kynema::interfaces::components::AerodynamicBody::delta_s

id

size_t kynema::interfaces::components::AerodynamicBody::id

jacobian_xi

std::vector<double> kynema::interfaces::components::AerodynamicBody::jacobian_xi

loads

std::vector<std::array<double, 6> > kynema::interfaces::components::AerodynamicBody::loads

motion_interp

std::vector<double> kynema::interfaces::components::AerodynamicBody::motion_interp

node_f

std::vector<std::array<double, 6> > kynema::interfaces::components::AerodynamicBody::node_f

node_ids

std::vector<size_t> kynema::interfaces::components::AerodynamicBody::node_ids

node_u

std::vector<std::array<double, 7> > kynema::interfaces::components::AerodynamicBody::node_u

node_v

std::vector<std::array<double, 6> > kynema::interfaces::components::AerodynamicBody::node_v

polar_size

std::vector<size_t> kynema::interfaces::components::AerodynamicBody::polar_size

qqr_motion_map

std::vector<std::array<double, 4> > kynema::interfaces::components::AerodynamicBody::qqr_motion_map

ref_axis_moments

std::vector<std::array<double, 3> > kynema::interfaces::components::AerodynamicBody::ref_axis_moments

shape_deriv_jac

std::vector<double> kynema::interfaces::components::AerodynamicBody::shape_deriv_jac

twist

std::vector<double> kynema::interfaces::components::AerodynamicBody::twist

u_motion_map

std::vector<std::array<double, 7> > kynema::interfaces::components::AerodynamicBody::u_motion_map

v_inflow

std::vector<std::array<double, 3> > kynema::interfaces::components::AerodynamicBody::v_inflow

v_motion

std::vector<std::array<double, 3> > kynema::interfaces::components::AerodynamicBody::v_motion

v_motion_map

std::vector<std::array<double, 6> > kynema::interfaces::components::AerodynamicBody::v_motion_map

v_rel

std::vector<std::array<double, 3> > kynema::interfaces::components::AerodynamicBody::v_rel

x_motion

std::vector<std::array<double, 3> > kynema::interfaces::components::AerodynamicBody::x_motion

xr_motion_map

std::vector<std::array<double, 7> > kynema::interfaces::components::AerodynamicBody::xr_motion_map

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The documentation for this class was generated from the following files:

• /home/runner/work/kynema/kynema/kynema/src/interfaces/components/aerodynamics.hpp
• /home/runner/work/kynema/kynema/kynema/src/interfaces/components/aerodynamics.cpp