Nodal Result of RS Table

 

 

Check the inertia forces and accelerations from response spectrum analysis at each node of a structure in a spreadsheet format table.

Table Tool in midas Civil offers a variety of powerful built-in functions. Refer to the following items for detail directions:

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Basic directions (Cell motion, selection, size control, etc.)

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Results Table

 

 

 

From the Main Menu select Results > Result Tables > Nodal Result of RS.

 

 

Refer to "Nodal Result of RS "

Select a vibration mode for which natural vibration vector will be produced, in the Records Activation Dialog.

In order to display inertia forces and accelerations due to modal combination, select Load Cases only. In order to display inertia forces and accelerations for each mode, select Load Cases and relevant Modes.

Refer to Usage of Table Tool and check the following data:

Results due to modal combination

Load Case: Response Spectrum Load Case

Modal Com.: Modal combination method

Node: Node of a structure

FX, FY, FZ: Nodal inertia force in each direction

MX, MY, MZ: Nodal bending moment in each direction

  Mb: Warping moment

DX, DY, DZ: Nodal acceleration in each direction

RX, RY, RZ: Nodal rotational acceleration in each direction

  RW: Warping acceleration

 

Results due to mode selection

Load Case: Response Spectrum Load Case

Mode: Mode selected in the Records Activation Dialog

Node: Node of a structure

FX, FY, FZ: Nodal inertia force in each direction

MX, MY, MZ: Nodal bending moment in each direction

Mb: Warping moment

DX, DY, DZ: Nodal acceleration in each direction

RX, RY, RZ: Nodal rotational acceleration in each direction

RW: Warping acceleration

Note 1

Inertial forces resulting from response spectrum analysis can be converted to nodal loads in the specified load case. The procedure is as follows:

 

Note 2

When Lumped Mass is selected in Structure Type, inertial force is calculated by Nodal Mass * Base Acceleration.  

When Consistent Mass is selected in Structure Type and floor diaphragm is considered, inertial forces of slave nodes will be transferred into that of master node. Therefore inertial forces of slave nodes will be displayed as zero in the table. If there is no  generated node in the master node position, inertial forces of all nodes will be displayed as zero.

When Consistent Mass is selected in Structure Type and floor diaphragm is not considered, inertial forces will be calculated using diagonal components in mass matrix.