You can use a response spectrum analysis to estimate the peak response
(displacement, stress, etc.) of a structure to a particular base motion. The
method is only approximate, but it is often a useful, inexpensive method for
preliminary design studies. The response spectrum procedure is based on using a
subset of the modes of the system, which must first be extracted by using the
eigenfrequency extraction procedure (described in
Configuring a frequency procedure”).
For more information, see
Response spectrum analysis.
Display the Edit Step dialog box following the
procedure outlined in
Creating a step
(Procedure type:Linear perturbation;
Response spectrum), or
Editing a step.
On the Basic and Damping
tabbed pages, configure settings such as a damping coefficient and the methods
for combining multidirectional excitations as described in the following
procedures.
Configure settings on the Basic tabbed page
In the Edit Step dialog box, display the
Basic tabbed page.
In the Description field, enter a short
description of the analysis step.
Abaqus
stores the text that you enter in the output database, and the text is
displayed in the state block by the Visualization module.
Click the arrow to the right of the Excitations
field, and select a directional summation method.
For the following options,
Abaqus/Standard
sums the directional excitation components first and then performs the modal
summation:
Select Single direction to sum the
directional excitation components for a single direction algebraically.
Select Multiple direction absolute sum to
sum the directional excitation components for multiple directions
algebraically.
For the following options,
Abaqus/Standard
performs the modal summation first and then sums the directional excitation
components:
Select Multiple direction square root of the sum of
squares to sum the directional excitation components for multiple
directions using the square root of the sum of the squares.
Select Multiple direction thirty percent
rule to sum the directional excitation components for multiple
directions using the 30% rule.
Select Multiple direction forty percent
rule to sum the directional excitation components for multiple
directions using the 40% rule.
Click the arrow to the right of the Summations
field, and select a modal summation method. For information on each of the
methods, see
Modal summation methods.
On the First direction tabbed page (and on the
Second direction and Third direction
tabbed pages if applicable), do the following:
In the Use response spectrum field, select
the spectrum amplitude to use for calculating the response. Alternatively, you
can click
to create a new amplitude. (See
Defining a spectrum,”
for more information.)
Enter Direction cosines X,
Y, and Z.
In the Scale factor field, enter the factor
multiplying the magnitudes in the response spectrum.
In the Time duration field, enter the time
duration of the dynamic event from which the spectrum was created. This setting
is applicable only when the Double sum combination modal
summation method is specified.
For multiple direction excitations, you have the option of toggling
on Apply third direction on the Third
direction tabbed page to include data for a third direction.
Configure settings on the Damping tabbed
page
In the Edit Step dialog box, display the
Damping tabbed page.
Choose Specify damping over ranges of Modes
to provide damping values for specific mode ranges.
Choose Specify damping over ranges of
Frequencies to provide damping values at specific frequencies.
Abaqus/Standard
interpolates the damping coefficient for a mode linearly between the specified
frequencies
If you omit damping data on the Damping tabbed
page,
Abaqus/Standard
assumes zero damping values. For more information, see
Specifying damping.
If you selected Modes in Step 2, select one or
more of the following options for defining damping:
Display the Direct modal tabbed page to
specify the fraction of critical damping, ,
for a particular mode range. Do the following:
Toggle on Use direct damping data.
Enter the following in the data table:
Start Mode: the mode number of the
lowest mode of a range.
End Mode: the mode number of the
highest mode of a range.
Critical Damping Fraction: fraction
of critical damping, .
Display the Composite modal tabbed page to
select composite modal damping using the damping coefficients calculated in the
preceding frequency step. (The damping calculations performed in the frequency
step are performed using damping data provided in the material definition.) Do
the following:
Toggle on Use composite damping data.
Enter the following in the data table:
Start Mode: the mode number of the
lowest mode of a range.
End Mode: the mode number of the
highest mode of a range.
Display the Rayleigh tabbed page to define
Rayleigh damping, and do the following:
Toggle on Use Rayleigh damping data.
Enter the following in the data table:
Start Mode: the mode number of the
lowest mode of a range.
End Mode: the mode number of the
highest mode of a range.