Description
Classical Timoshenko beam element with two nodes, and tapered sections.
For this tapered beam element, the averaged section properties are used to formulate the mass, stiffness and damping matrices. Note that there are also ChElementCableANCF if no torsional effects are needed, as in cables.
#include <ChElementBeamTaperedTimoshenko.h>
Public Member Functions | |
| virtual unsigned int | GetNumNodes () override |
| Get the number of nodes used by this element. | |
| virtual unsigned int | GetNumCoordsPosLevel () override |
| Get the number of coordinates in the field used by the referenced nodes. More... | |
| virtual unsigned int | GetNodeNumCoordsPosLevel (unsigned int n) override |
| Get the number of coordinates from the specified node that are used by this element. More... | |
| virtual std::shared_ptr< ChNodeFEAbase > | GetNode (unsigned int n) override |
| Access the nth node. | |
| virtual void | SetNodes (std::shared_ptr< ChNodeFEAxyzrot > nodeA, std::shared_ptr< ChNodeFEAxyzrot > nodeB) |
| void | SetTaperedSection (std::shared_ptr< ChBeamSectionTaperedTimoshenkoAdvancedGeneric > my_material) |
| Set the tapered section & material of beam element . | |
| std::shared_ptr< ChBeamSectionTaperedTimoshenkoAdvancedGeneric > | GetTaperedSection () |
| Get the tapered section & material of the element. | |
| std::shared_ptr< ChNodeFEAxyzrot > | GetNodeA () |
| Get the first node (beginning) | |
| std::shared_ptr< ChNodeFEAxyzrot > | GetNodeB () |
| Get the second node (ending) | |
| void | SetNodeAreferenceRot (ChQuaternion<> mrot) |
| Set the reference rotation of nodeA respect to the element rotation. | |
| ChQuaternion | GetNodeAreferenceRot () |
| Get the reference rotation of nodeA respect to the element rotation. | |
| void | SetNodeBreferenceRot (ChQuaternion<> mrot) |
| Set the reference rotation of nodeB respect to the element rotation. | |
| ChQuaternion | GetNodeBreferenceRot () |
| Get the reference rotation of nodeB respect to the element rotation. | |
| ChQuaternion | GetAbsoluteRotation () |
| Get the absolute rotation of element in space This is not the same of Rotation() , that expresses the accumulated rotation from starting point. | |
| ChQuaternion | GetRefRotation () |
| Get the original reference rotation of element in space. | |
| void | SetDisableCorotate (bool md) |
| Set this as true to have the beam behave like a non-corotated beam hence do not update the corotated reference. More... | |
| void | SetForceSymmetricStiffness (bool md) |
| Set this as true to force the tangent stiffness matrix to be inexact, but symmetric. More... | |
| void | SetUseGeometricStiffness (bool md) |
| Set this as false to disable the contribution of geometric stiffness to the total tangent stiffness. More... | |
| void | SetUseRc (bool md) |
| Set this as true to include the transformation matrix due to the different elastic center offsets at two ends of beam element with respect to the centerline reference, in which case the connection line of two elastic centers is not parallel to the one of two centerline references at two ends. More... | |
| void | SetUseRs (bool md) |
| Set this as true to include the transformation matrix due to the different shear center offsets at two ends of beam element with respect to the centerline reference, in which case the connection line of two shear centers is not parallel to the one of two centerline references at two ends. More... | |
| void | SetUseSimplifiedCorrectionForInclinedShearAxis (bool md) |
| Set this as true to use a simplified correction model for the case of inclined shear axis. More... | |
| void | ShapeFunctionsTimoshenko (ShapeFunctionGroup &NN, double eta) |
| Shape functions for Timoshenko beam. More... | |
| virtual void | Update () override |
| Update, called at least at each time step. More... | |
| virtual void | UpdateRotation () override |
| Compute large rotation of element for corotational approach The reference frame of this Euler-Bernoulli beam has X aligned to two nodes and Y parallel to Y of 1st node. | |
| virtual void | GetStateBlock (ChVectorDynamic<> &mD) override |
| Fills the D vector with the current field values at the nodes of the element, with proper ordering. More... | |
| void | GetFieldDt (ChVectorDynamic<> &mD_dt) |
| Fills the Ddt vector with the current time derivatives of field values at the nodes of the element, with proper ordering. More... | |
| void | GetFieldDt2 (ChVectorDynamic<> &mD_dtdt) |
| Fills the Ddtdt vector with the current time derivatives of field values at the nodes of the element, with proper ordering. More... | |
| virtual void | ComputeNodalMass () override |
| Add contribution of element inertia to total nodal masses. | |
| void | ComputeStiffnessMatrix () |
| Computes the local (material) stiffness matrix of the element: K = integral( [B]' * [D] * [B] ), Note: in this 'basic' implementation, constant section and constant material are assumed, so the explicit result of quadrature is used. More... | |
| void | ComputeDampingMatrix () |
| Computes the local (material) damping matrix of the element: R = beta * integral( [B]' * [D] * [B] ), Note: in this 'basic' implementation, constant section and constant material are assumed, so the explicit result of quadrature is used. More... | |
| void | ComputeGeometricStiffnessMatrix () |
| Computes the local geometric stiffness Kg of the element. More... | |
| void | ComputeAccurateTangentStiffnessMatrix (ChMatrixRef Kt_accurate, double Km_factor=1.0, double Kg_factor=1.0) |
| Computes the accurate tangent stiffness matrix of the element according to the paper: C A Felippa, B Haugen. More... | |
| void | ComputeKiRimatricesLocal (bool inertial_damping, bool inertial_stiffness) |
| Compute the inertia stiffness matrix [Ki^] and inertial damping matrix [Ri^] which are due to the gyroscopic effect. | |
| virtual void | ComputeKRMmatricesGlobal (ChMatrixRef H, double Kfactor, double Rfactor=0, double Mfactor=0) override |
| Sets H as the global stiffness matrix K, scaled by Kfactor. More... | |
| virtual void | GetKRMmatricesLocal (ChMatrixRef H, double Kmfactor, double Kgfactor, double Rmfactor, double Mfactor) |
| Gets the material mass, material stiffness, material damping and geometric stiffness matrices in local basis. More... | |
| virtual void | ComputeInternalForces (ChVectorDynamic<> &Fi) override |
| Computes the internal forces (e.g. More... | |
| virtual void | ComputeInternalForces (ChVectorDynamic<> &Fi, bool Mfactor, bool Kfactor, bool Rfactor, bool Gfactor) |
| Computes the inertial forces, damping forces, centrifugal forces and gyroscopic moments, then you could consider them as applied external forces, if you want to do the static solve when including nodal velocites and accelarations. More... | |
| virtual void | ComputeGravityForces (ChVectorDynamic<> &Fg, const ChVector3d &G_acc) override |
| Compute gravity forces, grouped in the Fg vector, one node after the other. More... | |
| virtual void | EvaluateSectionDisplacement (const double eta, ChVector3d &u_displ, ChVector3d &u_rotaz) override |
| Gets the xyz displacement of a point on the beam line, and the rotation RxRyRz of section plane, at abscyssa 'eta'. More... | |
| virtual void | EvaluateSectionFrame (const double eta, ChVector3d &point, ChQuaternion<> &rot) override |
| Gets the absolute xyz position of a point on the beam line, and the absolute rotation of section plane, at abscissa 'eta'. More... | |
| virtual void | EvaluateSectionForceTorque (const double eta, ChVector3d &Fforce, ChVector3d &Mtorque) override |
| Gets the force (traction x, shear y, shear z) and the torque (torsion on x, bending on y, on bending on z) at a section along the beam line, at abscissa 'eta'. More... | |
| virtual void | EvaluateSectionStrain (const double eta, ChVector3d &StrainV) override |
| Gets the axial and bending strain of the ANCF "cable" element. | |
| virtual void | EvaluateSectionStrain (const double eta, ChVector3d &StrainV_trans, ChVector3d &StrainV_rot) |
| Gets the strains(traction along x, shear along y, along shear z, torsion about x, bending about y, on bending about z) at a section along the beam line, at abscissa 'eta'. More... | |
| virtual void | EvaluateElementStrainEnergy (ChVector3d &StrainEnergyV_trans, ChVector3d &StrainEnergyV_rot) |
| Gets the elastic strain energy(traction along x, shear along y, along shear z, torsion about x, bending about y, on bending about z) in the element. | |
| virtual void | EvaluateElementDampingEnergy (ChVector3d &DampingEnergyV_trans, ChVector3d &DampingEnergyV_rot) |
| Gets the damping dissipated energy(traction along x, shear along y, along shear z, torsion about x, bending about y, on bending about z) in the element. | |
| virtual unsigned int | GetLoadableNumCoordsPosLevel () override |
| Gets the number of DOFs affected by this element (position part) | |
| virtual unsigned int | GetLoadableNumCoordsVelLevel () override |
| Gets the number of DOFs affected by this element (speed part) | |
| virtual void | LoadableGetStateBlockPosLevel (int block_offset, ChState &mD) override |
| Gets all the DOFs packed in a single vector (position part) | |
| virtual void | LoadableGetStateBlockVelLevel (int block_offset, ChStateDelta &mD) override |
| Gets all the DOFs packed in a single vector (speed part) | |
| virtual void | LoadableStateIncrement (const unsigned int off_x, ChState &x_new, const ChState &x, const unsigned int off_v, const ChStateDelta &Dv) override |
| Increment all DOFs using a delta. | |
| virtual unsigned int | GetNumFieldCoords () override |
| Number of coordinates in the interpolated field, ex=3 for a tetrahedron finite element or a cable, = 1 for a thermal problem, etc. | |
| virtual unsigned int | GetNumSubBlocks () override |
| Get the number of DOFs sub-blocks. | |
| virtual unsigned int | GetSubBlockOffset (unsigned int nblock) override |
| Get the offset of the specified sub-block of DOFs in global vector. | |
| virtual unsigned int | GetSubBlockSize (unsigned int nblock) override |
| Get the size of the specified sub-block of DOFs in global vector. | |
| virtual bool | IsSubBlockActive (unsigned int nblock) const override |
| Check if the specified sub-block of DOFs is active. | |
| virtual void | LoadableGetVariables (std::vector< ChVariables * > &mvars) override |
| Get the pointers to the contained ChVariables, appending to the mvars vector. | |
| virtual void | ComputeNF (const double U, ChVectorDynamic<> &Qi, double &detJ, const ChVectorDynamic<> &F, ChVectorDynamic<> *state_x, ChVectorDynamic<> *state_w) override |
| Evaluate N'*F , where N is some type of shape function evaluated at U coordinates of the line, each ranging in -1..+1 F is a load, N'*F is the resulting generalized load Returns also det[J] with J=[dx/du,..], that might be useful in gauss quadrature. More... | |
| virtual void | ComputeNF (const double U, const double V, const double W, ChVectorDynamic<> &Qi, double &detJ, const ChVectorDynamic<> &F, ChVectorDynamic<> *state_x, ChVectorDynamic<> *state_w) override |
| Evaluate N'*F , where N is some type of shape function evaluated at U,V,W coordinates of the volume, each ranging in -1..+1 F is a load, N'*F is the resulting generalized load Returns also det[J] with J=[dx/du,..], that might be useful in gauss quadrature. More... | |
| virtual double | GetDensity () override |
| This is needed so that it can be accessed by ChLoaderVolumeGravity. | |
 Public Member Functions inherited from chrono::fea::ChElementBeam | |
| double | GetMass () |
| The full mass of the beam, (with const. section, density, etc.) | |
| double | GetRestLength () |
| The rest length of the bar. | |
| void | SetRestLength (double ml) |
| Set the rest length of the bar (usually this should be automatically done when SetupInitial is called on beams element, given the current state, but one might need to override this, ex for precompressed beams etc). | |
| Public Member Functions inherited from chrono::fea::ChElementGeneric | |
| ChKRMBlock & | Kstiffness () |
| Access the proxy to stiffness, for sparse solver. | |
| virtual void | EleIntLoadResidual_F (ChVectorDynamic<> &R, const double c) override |
| Add the internal forces (pasted at global nodes offsets) into a global vector R, multiplied by a scaling factor c, as R += forces * c This default implementation is SLIGHTLY INEFFICIENT. | |
| virtual void | EleIntLoadResidual_Mv (ChVectorDynamic<> &R, const ChVectorDynamic<> &w, const double c) override |
| Add the product of element mass M by a vector w (pasted at global nodes offsets) into a global vector R, multiplied by a scaling factor c, as R += M * w * c This default implementation is VERY INEFFICIENT. | |
| virtual void | EleIntLoadLumpedMass_Md (ChVectorDynamic<> &Md, double &error, const double c) override |
| Adds the lumped mass to a Md vector, representing a mass diagonal matrix. More... | |
| virtual void | EleIntLoadResidual_F_gravity (ChVectorDynamic<> &R, const ChVector3d &G_acc, const double c) override |
| Add the contribution of gravity loads, multiplied by a scaling factor c, as: R += M * g * c This default implementation is VERY INEFFICIENT. More... | |
| virtual void | ComputeMmatrixGlobal (ChMatrixRef M) override |
| Calculate the mass matrix, expressed in global reference. More... | |
| virtual void | InjectKRMMatrices (ChSystemDescriptor &descriptor) override |
| Register with the given system descriptor any ChKRMBlock objects associated with this item. | |
| virtual void | LoadKRMMatrices (double Kfactor, double Rfactor, double Mfactor) override |
| Compute and load current stiffnes (K), damping (R), and mass (M) matrices in encapsulated ChKRMBlock objects. More... | |
| virtual void | VariablesFbLoadInternalForces (double factor=1.) override |
| Add the internal forces, expressed as nodal forces, into the encapsulated ChVariables. | |
| virtual void | VariablesFbIncrementMq () override |
| Add M*q (internal masses multiplied current 'qb'). | |
| Public Member Functions inherited from chrono::fea::ChElementBase | |
| virtual unsigned int | GetNumCoordsPosLevelActive () |
| Get the actual number of active degrees of freedom. More... | |
| virtual unsigned int | GetNodeNumCoordsPosLevelActive (unsigned int n) |
| Get the actual number of active coordinates from the specified node that are used by this element. More... | |
| virtual void | EleDoIntegration () |
| This is optionally implemented if there is some internal state that requires integration. | |
| Public Member Functions inherited from chrono::ChLoadableUVW | |
| virtual bool | IsTetrahedronIntegrationNeeded () |
| If true, use quadrature over u,v,w in [0..1] range as tetrahedron volumetric coords (with z=1-u-v-w) otherwise use default quadrature over u,v,w in [-1..+1] as box isoparametric coords. | |
| virtual bool | IsTrianglePrismIntegrationNeeded () |
| If true, use quadrature over u,v in [0..1] range as triangle natural coords (with z=1-u-v), and use linear quadrature over w in [-1..+1], otherwise use default quadrature over u,v,w in [-1..+1] as box isoparametric coords. | |
| Public Member Functions inherited from chrono::fea::ChElementCorotational | |
| ChMatrix33 & | Rotation () |
| Access the cumulative rotation matrix of the element. More... | |
Protected Member Functions | |
| virtual void | SetupInitial (ChSystem *system) override |
| Initial setup. More... | |
| void | ComputeTransformMatrix () |
| compute the transformation matrix due to offset and rotation of axes. | |
| void | ComputeTransformMatrixAtPoint (ChMatrixDynamic<> &mT, const double eta) |
| compute the transformation matrix due to offset and rotation of axes, at dimensionless abscissa eta. | |
Protected Attributes | |
| std::vector< std::shared_ptr< ChNodeFEAxyzrot > > | nodes |
| std::shared_ptr< ChBeamSectionTaperedTimoshenkoAdvancedGeneric > | tapered_section |
| Tapered section & material of beam element. | |
| ChMatrixDynamic | Km |
| local material stiffness matrix | |
| ChMatrixDynamic | Kg |
| local geometric stiffness matrix NORMALIZED by P | |
| ChMatrixDynamic | M |
| local material mass matrix. More... | |
| ChMatrixDynamic | Rm |
| local material damping matrix | |
| ChMatrixDynamic | Ri |
| local inertial-damping (gyroscopic damping) matrix | |
| ChMatrixDynamic | Ki |
| local inertial-stiffness matrix | |
| ChQuaternion | q_refrotA |
| ChQuaternion | q_refrotB |
| ChQuaternion | q_element_abs_rot |
| ChQuaternion | q_element_ref_rot |
| bool | disable_corotate |
| bool | force_symmetric_stiffness |
| bool | use_geometric_stiffness |
| whether include geometric stiffness matrix | |
| bool | use_Rc |
| whether use the transformation matrix for elastic axis orientation | |
| bool | use_Rs |
| whether use the transformation matrix for shear axis orientation | |
| bool | use_simplified_correction_for_inclined_shear_axis |
| whether use the simplified correction model for shear axis orientation, it's false as default. More... | |
| ChMatrixDynamic | T |
| transformation matrix for entire beam element | |
| ChMatrixDynamic | Rc |
| transformation matrix for elastic axis orientation | |
| ChMatrixDynamic | Rs |
| transformation matrix for shear axis orientation | |
| Protected Attributes inherited from chrono::fea::ChElementBeam | |
| double | mass |
| double | length |
| Protected Attributes inherited from chrono::fea::ChElementGeneric | |
| ChKRMBlock | Kmatr |
| Protected Attributes inherited from chrono::fea::ChElementCorotational | |
| ChMatrix33 | A |
Member Function Documentation
◆ ComputeAccurateTangentStiffnessMatrix()
| void chrono::fea::ChElementBeamTaperedTimoshenko::ComputeAccurateTangentStiffnessMatrix | ( | ChMatrixRef | Kt_accurate, |
| double | Km_factor = 1.0, |
||
| double | Kg_factor = 1.0 |
||
| ) |
Computes the accurate tangent stiffness matrix of the element according to the paper: C A Felippa, B Haugen.
A unified formulation of small strain corotational finite elements, I. Theory. 2005.
◆ ComputeDampingMatrix()
| void chrono::fea::ChElementBeamTaperedTimoshenko::ComputeDampingMatrix | ( | ) |
Computes the local (material) damping matrix of the element: R = beta * integral( [B]' * [D] * [B] ), Note: in this 'basic' implementation, constant section and constant material are assumed, so the explicit result of quadrature is used.
Also, this local material damping matrix is constant, computed only at the beginning for performance reasons; if you later change some material property, call this or InitialSetup(). Only the stiffness term(beta) is used for this implemented Rayleigh damping model.
◆ ComputeGeometricStiffnessMatrix()
| void chrono::fea::ChElementBeamTaperedTimoshenko::ComputeGeometricStiffnessMatrix | ( | ) |
Computes the local geometric stiffness Kg of the element.
Note: this->Kg will be set as the geometric stiffness EXCLUDING the multiplication by the P pull force, in fact P multiplication happens in all terms, thus this allows making the Kg as a constant matrix that is computed only at the beginning, and later it is multiplied by P all times the real Kg is needed. If you later change some material property, call this or InitialSetup().
◆ ComputeGravityForces()
|
overridevirtual |
Compute gravity forces, grouped in the Fg vector, one node after the other.
TODO for the lumped mass matrix case, the mM * mG product can be unrolled into few multiplications as mM mostly zero, and same for mG
Reimplemented from chrono::fea::ChElementGeneric.
◆ ComputeInternalForces() [1/2]
|
overridevirtual |
Computes the internal forces (e.g.
the actual position of nodes is not in relaxed reference position) and set values in the Fi vector. This functionality can be used to output the forces and torques at two nodes directly.
Implements chrono::fea::ChElementBase.
◆ ComputeInternalForces() [2/2]
|
virtual |
Computes the inertial forces, damping forces, centrifugal forces and gyroscopic moments, then you could consider them as applied external forces, if you want to do the static solve when including nodal velocites and accelarations.
Strictly speaking, it is not static solve any more. We can name it as quasi-static equilibrium solving, just the same as Simpack. It is recommended to use ChStaticNonLinearRheonomicAnalysis to do this kind of quasi-static equilibrium solving in case of rotating beams.
◆ ComputeKRMmatricesGlobal()
|
overridevirtual |
Sets H as the global stiffness matrix K, scaled by Kfactor.
Optionally, also superimposes global damping matrix R, scaled by Rfactor, and global mass matrix M multiplied by Mfactor.
< current angular velocity of section of node A, in material frame
< current angular acceleration of section of node A, in material frame
< current acceleration of section of node A, in material frame)
< current angular velocity of section of node B, in material frame
< current angular acceleration of section of node B, in material frame
< current acceleration of section of node B, in material frame
Implements chrono::fea::ChElementBase.
◆ ComputeNF() [1/2]
|
overridevirtual |
Evaluate N'*F , where N is some type of shape function evaluated at U coordinates of the line, each ranging in -1..+1 F is a load, N'*F is the resulting generalized load Returns also det[J] with J=[dx/du,..], that might be useful in gauss quadrature.
- Parameters
-
U parametric coordinate in line Qi Return result of Q = N'*F here detJ Return det[J] here F Input F vector, size is =n. field coords. state_x if != 0, update state (pos. part) to this, then evaluate Q state_w if != 0, update state (speed part) to this, then evaluate Q
Implements chrono::ChLoadableU.
Reimplemented in chrono::fea::ChElementBeamTaperedTimoshenkoFPM.
◆ ComputeNF() [2/2]
|
overridevirtual |
Evaluate N'*F , where N is some type of shape function evaluated at U,V,W coordinates of the volume, each ranging in -1..+1 F is a load, N'*F is the resulting generalized load Returns also det[J] with J=[dx/du,..], that might be useful in gauss quadrature.
- Parameters
-
U parametric coordinate in volume V parametric coordinate in volume W parametric coordinate in volume Qi Return result of N'*F here, maybe with offset block_offset detJ Return det[J] here F Input F vector, size is = n.field coords. state_x if != 0, update state (pos. part) to this, then evaluate Q state_w if != 0, update state (speed part) to this, then evaluate Q
Implements chrono::ChLoadableUVW.
Reimplemented in chrono::fea::ChElementBeamTaperedTimoshenkoFPM.
◆ ComputeStiffnessMatrix()
| void chrono::fea::ChElementBeamTaperedTimoshenko::ComputeStiffnessMatrix | ( | ) |
Computes the local (material) stiffness matrix of the element: K = integral( [B]' * [D] * [B] ), Note: in this 'basic' implementation, constant section and constant material are assumed, so the explicit result of quadrature is used.
Also, this local material stiffness matrix is constant, computed only at the beginning for performance reasons; if you later change some material property, call this or InitialSetup().
◆ EvaluateSectionDisplacement()
|
overridevirtual |
Gets the xyz displacement of a point on the beam line, and the rotation RxRyRz of section plane, at abscyssa 'eta'.
Note, eta=-1 at node1, eta=+1 at node2. Results are not corotated.
Implements chrono::fea::ChElementBeam.
Reimplemented in chrono::fea::ChElementBeamTaperedTimoshenkoFPM.
◆ EvaluateSectionForceTorque()
|
overridevirtual |
Gets the force (traction x, shear y, shear z) and the torque (torsion on x, bending on y, on bending on z) at a section along the beam line, at abscissa 'eta'.
Note, eta=-1 at node1, eta=+1 at node2. Results are not corotated, and are expressed in the reference system of beam.
Implements chrono::fea::ChElementBeam.
Reimplemented in chrono::fea::ChElementBeamTaperedTimoshenkoFPM.
◆ EvaluateSectionFrame()
|
overridevirtual |
Gets the absolute xyz position of a point on the beam line, and the absolute rotation of section plane, at abscissa 'eta'.
Note, eta=-1 at node1, eta=+1 at node2. Results are corotated (expressed in world reference)
Implements chrono::fea::ChElementBeam.
◆ EvaluateSectionStrain()
|
virtual |
Gets the strains(traction along x, shear along y, along shear z, torsion about x, bending about y, on bending about z) at a section along the beam line, at abscissa 'eta'.
It's evaluated at the elastic center. Note, eta=-1 at node1, eta=+1 at node2. Results are not corotated, and are expressed in the reference system of beam.
Reimplemented in chrono::fea::ChElementBeamTaperedTimoshenkoFPM.
◆ GetFieldDt()
| void chrono::fea::ChElementBeamTaperedTimoshenko::GetFieldDt | ( | ChVectorDynamic<> & | mD_dt | ) |
Fills the Ddt vector with the current time derivatives of field values at the nodes of the element, with proper ordering.
If the D vector has not the size of this->GetNumCoordsPosLevel(), it will be resized. For corotational elements, field is assumed in local reference! Give that this element includes rotations at nodes, this gives: {v_a v_a v_a wx_a wy_a wz_a v_b v_b v_b wx_b wy_b wz_b}
◆ GetFieldDt2()
| void chrono::fea::ChElementBeamTaperedTimoshenko::GetFieldDt2 | ( | ChVectorDynamic<> & | mD_dtdt | ) |
Fills the Ddtdt vector with the current time derivatives of field values at the nodes of the element, with proper ordering.
If the D vector has not the size of this->GetNumCoordsPosLevel(), it will be resized. For corotational elements, field is assumed in local reference! Give that this element includes rotations at nodes, this gives: {acc_a acc_a acc_a accx_a accy_a accz_a acc_b acc_b acc_b accx_b accy_b accz_b}
◆ GetKRMmatricesLocal()
|
virtual |
Gets the material mass, material stiffness, material damping and geometric stiffness matrices in local basis.
This functionality can be used to output these matrices for some other special needs.
◆ GetNodeNumCoordsPosLevel()
|
inlineoverridevirtual |
Get the number of coordinates from the specified node that are used by this element.
Note that this may be different from the value returned by GetNode(n)->GetNumCoordsVelLevel().
Implements chrono::fea::ChElementBase.
◆ GetNumCoordsPosLevel()
|
inlineoverridevirtual |
Get the number of coordinates in the field used by the referenced nodes.
This is for example the size (number of rows/columns) of the local stiffness matrix.
Implements chrono::fea::ChElementBase.
◆ GetStateBlock()
|
overridevirtual |
Fills the D vector with the current field values at the nodes of the element, with proper ordering.
If the D vector has not the size of this->GetNumCoordsPosLevel(), it will be resized. For corotational elements, field is assumed in local reference! Given that this element includes rotations at nodes, this gives: {x_a y_a z_a Rx_a Ry_a Rz_a x_b y_b z_b Rx_b Ry_b Rz_b}
Implements chrono::fea::ChElementBase.
◆ SetDisableCorotate()
|
inline |
Set this as true to have the beam behave like a non-corotated beam hence do not update the corotated reference.
Just for benchmarks!
◆ SetForceSymmetricStiffness()
|
inline |
Set this as true to force the tangent stiffness matrix to be inexact, but symmetric.
This allows the use of faster solvers. For systems close to the equilibrium, the tangent stiffness would be symmetric anyway.
◆ SetupInitial()
|
overrideprotectedvirtual |
Initial setup.
Precompute mass and matrices that do not change during the simulation, such as the local tangent stiffness Kl of each element, if needed, etc.
Reimplemented from chrono::fea::ChElementBase.
◆ SetUseGeometricStiffness()
|
inline |
Set this as false to disable the contribution of geometric stiffness to the total tangent stiffness.
By default it is on.
◆ SetUseRc()
|
inline |
Set this as true to include the transformation matrix due to the different elastic center offsets at two ends of beam element with respect to the centerline reference, in which case the connection line of two elastic centers is not parallel to the one of two centerline references at two ends.
By default it is on. Please refer to ANSYS theory document for more information.
◆ SetUseRs()
|
inline |
Set this as true to include the transformation matrix due to the different shear center offsets at two ends of beam element with respect to the centerline reference, in which case the connection line of two shear centers is not parallel to the one of two centerline references at two ends.
By default it is on. This transformation matrix could decrease the equivalent torsional stiffness of beam element, and hence generate larger torsional rotation. Please refer to ANSYS theory document for more information.
◆ SetUseSimplifiedCorrectionForInclinedShearAxis()
|
inline |
Set this as true to use a simplified correction model for the case of inclined shear axis.
By default it is false. This option may affect the bending-twist coupling of Timoshenko beam element, especially when the inclined angle of shear center axis is obvious with respect to the centerline.
◆ ShapeFunctionsTimoshenko()
| void chrono::fea::ChElementBeamTaperedTimoshenko::ShapeFunctionsTimoshenko | ( | ShapeFunctionGroup & | NN, |
| double | eta | ||
| ) |
Shape functions for Timoshenko beam.
Please refer to the textbook: J. S. Przemieniecki, Theory of Matrix Structural Analysis-Dover Publications (1985).
◆ Update()
|
overridevirtual |
Update, called at least at each time step.
If the element has to keep updated some auxiliary data, such as the rotation matrices for corotational approach, this should be implemented in this function.
Reimplemented from chrono::fea::ChElementBase.
Member Data Documentation
◆ M
|
protected |
local material mass matrix.
It could be lumped or consistent mass matrix, depending on SetLumpedMassMatrix(true/false)
◆ use_simplified_correction_for_inclined_shear_axis
|
protected |
whether use the simplified correction model for shear axis orientation, it's false as default.
The documentation for this class was generated from the following files:
- /builds/uwsbel/chrono/src/chrono/fea/ChElementBeamTaperedTimoshenko.h
- /builds/uwsbel/chrono/src/chrono/fea/ChElementBeamTaperedTimoshenko.cpp
