4.14.5.32. Pinching Limit State Material¶
This command is used to construct a uniaxial material that simulates a pinched load-deformation response and exhibits degradation under cyclic loading. This material works with the RotationShearCurve limit surface that can monitor a key deformation and/or a key force in an associated frame element and trigger a degrading behavior in this material when a limiting value of the deformation and/or force are reached. The material can be used in two modes: 1) direct input mode, where pinching and damage parameters are directly input; and 2) calibrated mode for shear-critical concrete columns, where only key column properties are input for model to fully define pinching and damage parameters.
- uniaxialMaterial('PinchingLimitStateMaterial', matTag, nodeT, nodeB, driftAxis, Kelas, crvTyp, crvTag, YpinchUPN, YpinchRPN, XpinchRPN, YpinchUNP, YpinchRNP, XpinchRNP, dmgStrsLimE, dmgDispMax, dmgE1, dmgE2, dmgE3, dmgE4, dmgELim, dmgR1, dmgR2, dmgR3, dmgR4, dmgRLim, dmgRCyc, dmgS1, dmgS2, dmgS3, dmgS4, dmgSLim, dmgSCyc)
MODE 1: Direct Input
matTag
(int)integer tag identifying material
nodeT
(int)integer node tag to define the first node at the extreme end of the associated flexural frame member (L3 or D5 in Figure)
nodeB
(int)integer node tag to define the last node at the extreme end of the associated flexural frame member (L2 or D2 in Figure)
driftAxis
(int)integer to indicate the drift axis in which lateral-strength degradation will occur. This axis should be orthogonal to the axis of measured rotation (see
rotAxis
in Rotation Shear Curve definition)driftAxis
= 1 - Drift along the x-axisdriftAxis
= 2 - Drift along the y-axisdriftAxis
= 3 - Drift along the z-axisKelas
(float)floating point value to define the initial material elastic stiffness (Kelastic); Kelas > 0
crvTyp
(int)integer flag to indicate the type of limit curve associated with this material.
crvTyp
= 0 - No limit curvecrvTyp
= 1 - axial limit curvecrvTyp
= 2 - RotationShearCurvecrvTag
(int)integer tag for the unique limit curve object associated with this material
YpinchUPN
(float)floating point unloading force pinching factor for loading in the negative direction. Note: This value must be between zero and unity
YpinchRPN
(float)floating point reloading force pinching factor for loading in the negative direction. Note: This value must be between negative one and unity
XpinchRPN
(float)floating point reloading displacement pinching factor for loading in the negative direction. Note: This value must be between negative one and unity
YpinchUNP
(float)floating point unloading force pinching factor for loading in the positive direction. Note: This value must be between zero and unity
YpinchRNP
(float)floating point reloading force pinching factor for loading in the positive direction. Note: This value must be between negative one and unity
XpinchRNP
(float)floating point reloading displacement pinching factor for loading in the positive direction. Note: This value must be between negative one and unity
dmgStrsLimE
(float)floating point force limit for elastic stiffness damage (typically defined as the lowest of shear strength or shear at flexrual yielding). This value is used to compute the maximum deformation at flexural yield (δmax Eq. 1) and using the initial elastic stiffness (Kelastic) the monotonic energy (Emono Eq. 1) to yield. Input 1 if this type of damage is not required and set
dmgE1
,dmgE2
,dmgE3
,dmgE4
, anddmgELim
to zerodmgDispMax
(float)floating point for ultimate drift at failure (δmax Eq. 1) and is used for strength and stiffness damage. This value is used to compute the monotonic energy at axial failure (Emono Eq. 2) by computing the area under the backbone in the positive loading direction up to δmax. Input 1 if this type of damage is not required and set
dmgR1
,dmgR2
,dmgR3
,dmgR4
, anddmgRLim
to zero for reloading stiffness damage. Similarly setdmgS1
,dmgS2
,dmgS3
,dmgS4
, anddmgSLim
to zero if reloading strength damage is not requireddmgE1
dmgE2
(float)floating point elastic stiffness damage factors α1,α2,α3,α4 shown in Eq. 1
dmgE3
dmgE4
(float)floating point elastic stiffness damage factors α1,α2,α3,α4 shown in Eq. 1
dmgELim
(float)floating point elastic stiffness damage limit Dlim shown in Eq. 1; Note: This value must be between zero and unity
dmgR1
dmgR2
(float)floating point reloading stiffness damage factors α1,α2,α3,α4 shown in Eq. 1
dmgR3
dmgR4
(float)floating point reloading stiffness damage factors α1,α2,α3,α4 shown in Eq. 1
dmgRLim
(float)floating point reloading stiffness damage limit Dlim shown in Eq. 1; Note: This value must be between zero and unity
dmgRCyc
(float)floating point cyclic reloading stiffness damage index; Note: This value must be between zero and unity
dmgS1
dmgS2
(float)floating point backbone strength damage factors α1,α2,α3,α4 shown in Eq. 1
dmgS3
dmgS4
(float)floating point backbone strength damage factors α1,α2,α3,α4 shown in Eq. 1
dmgSLim
(float)floating point backbone strength damage limit Dlim shown in Eq. 1; Note: This value must be between zero and unity
dmgSCyc
(float)floating point cyclic backbone strength damage index; Note: This value must be between zero and unity
- uniaxialMaterial('PinchingLimitStateMaterial', matTag, dnodeT, nodeB, driftAxis, Kelas, crvTyp, crvTag, eleTag, b, d, h, a, st, As, Acc, ld, db, rhot, fc, fy, fyt)
MODE 2: Calibrated Model for Shear-Critical Concrete Columns
matTag
(int)integer tag identifying material
nodeT
(int)integer node tag to define the first node at the extreme end of the associated flexural frame member (L3 or D5 in Figure)
nodeB
(int)integer node tag to define the last node at the extreme end of the associated flexural frame member (L2 or D2 in Figure)
driftAxis
(int)integer to indicate the drift axis in which lateral-strength degradation will occur. This axis should be orthogonal to the axis of measured rotation (see
rotAxis`
in Rotation Shear Curve definition)driftAxis
= 1 - Drift along the x-axisdriftAxis
= 2 - Drift along the y-axisdriftAxis
= 3 - Drift along the z-axisKelas
(float)floating point value to define the shear stiffness (Kelastic) of the shear spring prior to shear failure
Kelas
= -4 - Shear stiffness calculated assuming double curvature and shear springs at both column element endsKelas
= -3 - Shear stiffness calculated assuming double curvature and a shear spring at one column element endKelas
= -2 - Shear stiffness calculated assuming single curvature and shear springs at both column element endsKelas
= -1 - Shear stiffness calculated assuming single curvature and a shear spring at one column element endKelas
> 0 - Shear stiffness is the input valueNote: integer inputs allow the model to know whether column height equals the shear span (cantelever) or twice the shear span (double curvature). For columns in frames, input the value for the case that best approximates column end conditions or manually input shear stiffness (typically double curvature better estimates framed column behavior)
crvTag
(int)integer tag for the unique limit curve object associated with this material
eleTag
(int)integer element tag to define the associated beam-column element used to extract axial load
b
(float)floating point column width (inches)
d
(float)floating point column depth (inches)
h
(float)floating point column height (inches)
a
(float)floating point shear span length (inches)
st
(float)floating point transverse reinforcement spacing (inches) along column height
As
(float)floating point total area (inches squared) of longitudinal steel bars in section
Acc
(float)floating point gross confined concrete area (inches squared) bounded by the transverse reinforcement in column section
ld
(float)floating point development length (inches) of longitudinal bars using ACI 318-11 Eq. 12-1 and Eq. 12-2
db
(float)floating point diameter (inches) of longitudinal bars in column section
rhot
(float)floating point transverse reinforcement ratio (Ast/st.db)
f'c
(float)floating point concrete compressive strength (ksi)
fy
(float)floating point longitudinal steel yield strength (ksi)
fyt
(float)floating point transverse steel yield strength (ksi)
See also