Function GetStressTensorValuesForAllNodesOfElement( _
   ByVal ElementNumbers As System.Object, _
   ByVal NUnits As System.Integer, _
   ByVal NStepNum As System.Integer, _
   ByRef ErrorCode As System.Integer _
) As System.Object

Dim instance As ICWResults
Dim ElementNumbers As System.Object
Dim NUnits As System.Integer
Dim NStepNum As System.Integer
Dim ErrorCode As System.Integer
Dim value As System.Object
 
value = instance.GetStressTensorValuesForAllNodesOfElement(ElementNumbers, NUnits, NStepNum, ErrorCode)

System.object GetStressTensorValuesForAllNodesOfElement( 
   System.object ElementNumbers,
   System.int NUnits,
   System.int NStepNum,
   out System.int ErrorCode
)

System.Object^ GetStressTensorValuesForAllNodesOfElement( 
&   System.Object^ ElementNumbers,
&   System.int NUnits,
&   System.int NStepNum,
&   [Out] System.int ErrorCode
) 

Parameters

ElementNumbers

An array of mesh element numbers for which to return nodal results; specify the element number of a single element (see Remarks)

NUnits

Units as defined in swsStrengthUnit_e

NStepNum

Solution step number (use 1 for steady state)

ErrorCode

Error as defined in swsNodalResultsOfElementError_e

Return Value

This method is valid only for solid and shell meshes. Beam meshes are not supported.

Call ICWMesh::ElementCount to specify ElementNumbers.

The number of rows in the returned two-dimensional array is:

    (n * m * p) 

where:

• n = # elements in the mesh
• m = # nodes for each element
• p = 2 for shell meshes (top and bottom faces); 1 for solid meshes

Each row contains nine values:

    element_i, shell_face_i, node_i, tensor_value_1, tensor_value_2, tensor_value_3, tensor_value_4, tensor_value_5, tensor_value_6

where:

• element_i = the zero-based index of the element in the mesh
• shell_face_i = 0 for the top face of a shell mesh, 1 for the bottom face of a shell mesh, and -1 for a solid mesh
• node_i = the zero-based index of the node for this row's element

Therefore, the array returned for a shell mesh contains 18*n*m values in the following order:

[ 

   element_1, shell_face_0, node_1, tensor_value_1, tensor_value_2, tensor_value_3, tensor_value_4, tensor_value_5, tensor_value_6 

   element_1, shell_face_0, node_2, tensor_value_1, tensor_value_2, tensor_value_3, tensor_value_4, tensor_value_5, tensor_value_6

   ... 

   element_1, shell_face_0, node_m, tensor_value_1, tensor_value_2, tensor_value_3, tensor_value_4, tensor_value_5, tensor_value_6

   (repeat above for shell_face_1)

   (repeat above for element_2 through element_n)

]