GlobalPhysicalVariables Namespace Reference

Global physical variables. More...

Functions
Vector< double >	get_principal_stretches (const double &time, const double &r)
Vector< double >	get_principal_stretch_derivatives (const double &time, const double &r)
void	deformed_position_fct (const double &time, const Vector< double > &xi, Vector< double > &x)
void	deformed_velocity_fct (const double &time, const Vector< double > &xi, Vector< double > &x_dot)
void	deformed_accel_fct (const double &time, const Vector< double > &xi, Vector< double > &x_ddot)
void	body_force_fct (const double &time, const Vector< double > &xi, Vector< double > &b)
void	traction_force_fct (const double &time, const Vector< double > &xi, const Vector< double > &x, const Vector< double > &n, Vector< double > &traction)

Variables
double	nu = 0.4
double	A0 = 0.05
double	B0 = 0.05
double	omega = 5.0

Detailed Description

Global physical variables.

Function Documentation

body_force_fct()

void GlobalPhysicalVariables::body_force_fct	(	const double &	time,
		const Vector< double > &	xi,
		Vector< double > &	b
	)

Definition at line 125 of file shell_unsteady.cc.

References A0, B0, get_principal_stretch_derivatives(), get_principal_stretches(), nu, and omega.

Referenced by ShellProblem< ELEMENT >::complete_problem_setup().

deformed_accel_fct()

void GlobalPhysicalVariables::deformed_accel_fct	(	const double &	time,
		const Vector< double > &	xi,
		Vector< double > &	x_ddot
	)

Definition at line 112 of file shell_unsteady.cc.

References A0, B0, and omega.

Referenced by ShellProblem< ELEMENT >::set_initial_condition().

deformed_position_fct()

void GlobalPhysicalVariables::deformed_position_fct	(	const double &	time,
		const Vector< double > &	xi,
		Vector< double > &	x
	)

Definition at line 86 of file shell_unsteady.cc.

References A0, B0, and omega.

Referenced by ShellProblem< ELEMENT >::set_initial_condition().

deformed_velocity_fct()

void GlobalPhysicalVariables::deformed_velocity_fct	(	const double &	time,
		const Vector< double > &	xi,
		Vector< double > &	x_dot
	)

Definition at line 99 of file shell_unsteady.cc.

References A0, B0, and omega.

Referenced by ShellProblem< ELEMENT >::set_initial_condition().

get_principal_stretch_derivatives()

Vector< double > GlobalPhysicalVariables::get_principal_stretch_derivatives	(	const double &	time,
		const double &	r
	)

Definition at line 75 of file shell_unsteady.cc.

References B0, and omega.

Referenced by body_force_fct().

get_principal_stretches()

Vector< double > GlobalPhysicalVariables::get_principal_stretches	(	const double &	time,
		const double &	r
	)

Definition at line 64 of file shell_unsteady.cc.

References A0, B0, and omega.

Referenced by body_force_fct(), and traction_force_fct().

traction_force_fct()

void GlobalPhysicalVariables::traction_force_fct	(	const double &	time,
		const Vector< double > &	xi,
		const Vector< double > &	x,
		const Vector< double > &	n,
		Vector< double > &	traction
	)

Definition at line 161 of file shell_unsteady.cc.

References get_principal_stretches(), and nu.

Referenced by ShellProblem< ELEMENT >::complete_problem_setup().

Variable Documentation

A0

double GlobalPhysicalVariables::A0 = 0.05

Definition at line 57 of file shell_unsteady.cc.

Referenced by body_force_fct(), deformed_accel_fct(), deformed_position_fct(), deformed_velocity_fct(), and get_principal_stretches().

B0

double GlobalPhysicalVariables::B0 = 0.05

Definition at line 58 of file shell_unsteady.cc.

Referenced by body_force_fct(), deformed_accel_fct(), deformed_position_fct(), deformed_velocity_fct(), get_principal_stretch_derivatives(), and get_principal_stretches().

nu

double GlobalPhysicalVariables::nu = 0.4

Definition at line 54 of file shell_unsteady.cc.

Referenced by body_force_fct(), main(), ShellProblem< ELEMENT >::ShellProblem(), and traction_force_fct().

omega

double GlobalPhysicalVariables::omega = 5.0

Definition at line 61 of file shell_unsteady.cc.

Referenced by body_force_fct(), deformed_accel_fct(), deformed_position_fct(), deformed_velocity_fct(), get_principal_stretch_derivatives(), get_principal_stretches(), and ShellProblem< ELEMENT >::ShellProblem().