Pushover Analysis Procedure
using SAP2000
PART 2
Pushover Analysis in SAP2000:
Steps Sequence
1. Create the model.
2. Define frame hinges properties and assign them to the frame elements.
3. Define the parameters to calculate the demand for each performance level (f.e.: acceleration response spectra, ATC-40, FEMA; MRSA).
4. Define the load patterns which are needed for pushover: gravity loads and any other load acting on the structure before lateral seismic
loading.
5. Define the Non-Linear Static load cases and the Modal load case to be used for pushover analysis.
6. Run the Pushover load cases and check the results (Pushover curve). 7. Determine the target displacement by an appropriate method
(ATC-40, FEMA, other).
8. Evaluate the number and state of plastic hinges in the structure, and then check the maximum strains for the most critical hinge.
9. Change structural configuration (additional piles, modified pile layout) if needed and repeat the process.
Model Description
• Trestle 105 m length. • 7 spans 15 m length. • Bents with three steel
pipe (φ = 1.42 m) piles. • Steel box section cap
beam (H=1.20).
• 5 steel I-Wide section longitudinal beams.
• Concrete slab thickness = 0.30 m.
Discretization
soil-Mass Source Definition
• DEAD load.• Piping load (permanently attached equipment).
• 5KPa (10% of uniform live load)
• Vehicle load (part of the crane above the deck)
• MASS_ADD_MG
(additional mass due to marine growth)
• MASS_ADD_WATER
(Hydrodynamic mass internal and external to the pile)
Marine Growth Load
• Pile diameter Dp = 1.42 m • MG thk = 0.20 m
• MG γ = 12.75 KN/m3
Hydrodynamic Added Mass
• Pile diameter Dp = 1.42 m • Water γ = 9.81 KN/m3
Pile Moment-Curvature Analysis
• Three levels of axial load: P1 = -10000 KN (max compression), P2 = -1700 KN (DEAD load), P3 = 5000 (max tension).
Pile Moment-Curvature Analysis
Determination of the bilinear M-Phi diagram for:
P = -1700 KN Angle = 0°
Pile Moment-Curvature Analysis
• Bilinear M-Phi diagram for: P = -1700 KN, Angle = 0°Mne = 18700 KN-m Mp = 21000 KN-m Mp/Mne = 1.12 φY = 0.012 φu = 0.237 φp = φu – φY = 0.225 The same procedure should be repeated for the other two levels of axial force!
Pile Hinge Definition 3
Pile Hinge Definition 4
Pile Hinge Definition 5
Pile Hinge Definition 6
• Calculating the SF of the hinge PILE-ST52
To define the Moment-Curvature Curve of hinge PILE-ST52, it is
required to calculate the yielding curvature (SF) used by the program: SF = θy / Lp = 5.016E-3 / 1.5 = 3.344E-3
Pile Hinge Definition 7
Pile Hinge Definition 8
Pile Hinge Definition 9
• M-Phi curve definition for PILE-ST52
From bilinear M-Phi: Mp/Mne = 1.12
0.20 Mp/Mne = 0.22 φp = 0.225
SF = 3.344E-3 φp / SF = 67
Notice that only plastic curvatures over SF have to be specified in the right column. In the left column the Mp/Mne (obtained from M-Phi bilinear diagram) is assigned to point C and a 20% of that value to point D.
Due to numerical stability it is highly recommendable that line CD has a negative slope (not vertical) and line DE a positive slope (not horizontal).
Pile Hinge Definition 10
• Interaction surface definition for PILE-ST52
Automatically defined for each generated hinge.
It is only used to determine the exact yielding moment (Mne2, Mne3) and the angle of bending (tg α= Mne3 / Mne2).
1. The described procedure has to be repeated for the
definition of hinges in the cap beam and longitudinal
beam.
2. Due to the lower importance of beam hinges, they can
be defined faster by means of the “Automatic Hinges” if
the conditions for type of material and cross-section
geometry are met (See Part 1 of this guide).
3. It is very likely that in the hinge length for beams is not
the same as the total length of the frame element but a
fraction. This should be taken into account when defining
the hinge length (Lp) relative to the frame element
length. This is an important parameter for the correct
determination of the SF (yield curvature) from the yield
rotation automatically calculated by the program.
1. Sudden strength loss is not recommended (segment C-D)
2. Reduce the mesh size helps when using sudden strength
loss.
3. It is possible to define hinges along the whole frame
length (e.g.: 10 hinges spaced every tenth part of the
total length).
4. Repeat the described process for all the combinations of
bending angles and axial loads.
5. For bi-axial or asymmetrical cross-sections, define M-Phi
for intermediate bending angles (e.g.: 45°).
6. Once the plastic hinge definition is concluded (SF
calulated by the program determined), the property has
to be newly assigned to all the corresponding frames.
Parameters for ATC-40 Capacity-Spectrum
Method
Definition of response spectrum function (without scaling) for
each demand level (OLE-D1, CLE-D2, DE-D3)
Parameters for ATC-40 Capacity-Spectrum
Method
DEAD Load Case Definition
• Constitutes the starting point of pushover analysis.
• Non-linear geometric P-Delta analysis is performed for all the gravity loads present before earthquake
MODAL Load Case Definition
• The results of MODAL load case are used in the definition of the ATC-40 capacity spectrum (ADRS format) and the equivalent period required to obtain the performance point (target displacement).
• Besides, the mode shapes are used in the definition of the MODE load pattern for pushover analysis.
Pushover MODE Load Pattern
1. More critical pushover load pattern. Preferred
over uniform ACCEL load pattern.
2. Modal analysis has to be performed first.
3. The two fundamental modes with higher modal
mass participation in directions X and Y,
respectively, are selected for the definition of
MODE load pattern.
Pushover MODE Load Pattern
Pushover MODE Load Pattern
Pushover MODE Load Pattern
Pushover: Number of saved steps for
results analysis
1. Keep using the same type of geometric non-linearity (e.g.: P-Delta) through all the non-linear load case defined in the
model.
2. Start the model with as few hinges as possible. then gradually increment the number of hinges as necessary.
3. The first run may no include any type of geometric non-linearity. Then, after checking results and analysis
performance, add P-Delta and may be Large Displacements. 4. Start with modest target displacements and limited number
of steps (saved and total). The idea is always have the
possibility of first perform a quickly analysis. Afterwards the non-linear behavior could be incremented.
5. Consider more than two loading directions (or loading modes) to evaluate the structure under different loading situations.
Pushover Analysis:
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).
ATC-40 Capacity Spectrum display parameters.
D2 Performance Level.
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).
Target displacement. D2 Performance Level.
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).
ATC-40 Capacity Spectrum display parameters.
D3 Performance Level.
Besides the elastic period and damping ratio, the effective inelastic parameters are also displayed.
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).
Target displacement. D3 Performance Level.
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).
Load steps corresponding to target displacements.
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).Identification of first hinge that yields (hinge with maximum deformations through all the pushover analysis load history.)
First plastic in-ground hinge appears in the bottom part of the pile at load step 32
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).Extract information for yielding (step 32), level D2 (step 34) and level D3 (step 49)
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).Extract information for yielding (step 32), level D2 (step 34) and level D3 (step 49)
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).Yield curvature calculation
My = 11085 KN.m
Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).Pushover Results Analysis
Pushover in Y direction (Mode 1 load pattern).Tensile steel strain for level D2 and D3 are smaller than Strain limits for CLE and DE performance levels, respectively. Therefore, the
seismic capacity of the piles is verified.