Comments about your bas code:
*loop materials
*If(MatProp(consider_uniElastic,Int)!=0)*\
uniaxialMaterial Elastic *MatNum *MatProp(uni_E) *MatProp(uni_damping)
*endif
*End materials
1 ) *\ seems incorrect at the end of a *if command
2) loop materials make a loop over all materials assigned to entities. In
order to use *If(MatProp(consider_uniElastic,Int)!=0) must
be sure that all defined materials have a field named "consider_uniElastic",
and in your case other materials don't have this field !!!
You can create a field (can be hidden) defined for all materials to identify
before use other fields, for example
QUESTION: TypeId
VALUE: elastic
STATE: Hidden
Are you are sure that the field "uni_E" is really defined for all loops ??
Note: Some of your attached files are removed by the mail server antivirus,
please for further messages send a zip file with single extension.
Regards
Enrique Escolano
----- Original Message -----
From: "Esneyder Montoya"
esneyder.montoya at utoronto.ca
To:
gidlist at GATXAN.CIMNE.UPC.ES
Sent: Sunday, August 08, 2004 8:08 PM
Subject: [GiDlist] .bas problem
Warning: This message has had one or more attachments removed.
Warning: Please read the "VirusWarning.txt" attachment(s) for more
information.
Dear GiD Team
I have a problem when trying to run my project.gid files, a material
was set like:
BOOK: uniaxialMat
NUMBER: 11 MATERIAL: uniElastic
QUESTION:consider_uniElastic#CB#(0,1)
VALUE:0
QUESTION: uni_E:
VALUE:30000
QUESTION: uni_damping:
VALUE:0.0
END MATERIAL
.....
and in the project.bas file, the material is called as:
*loop materials
*If(MatProp(consider_uniElastic,Int)!=0)*\
uniaxialMaterial Elastic *MatNum *MatProp(uni_E) *MatProp(uni_damping)
*endif
*End materials
....
when trying to write the calculation file, I am having the following
error:
Error in base file C:\... at line number ...: word: 'uni_E' doesn't exist
In this case I am not selecting this particular material within the
problem am solving, so the *.bas file must actually pass over this
isntruction and do nothing, which is not the case.
Could you give me a hint on what might be the problem. I am attaching
the project files
----------------------------------------------------------------------------
----
###############################################################
# General purpose 3D-FEA #
# Using GID Pre-Processor For OpenSees #
# GID Problem type : EMOpenSEEs #
# Written by : Esneyder Montoya, Ph.D., P.Eng. #
# MontoyaE at mmm.ca #
# This file is a template for translating GID information #
# into OpenSees TCL input file #
# Date : July, 19, 2004 #
# Updated: July, 26, 2004 ##
#
###############################################################
#########################################################
# This file is created from GID pre- and post-processor #
# using "EMOpenSEEs.gid" Problem Type #
#########################################################
# ------------------------------
# Start of model generation
# ------------------------------
# Create ModelBuilder
*if(strcmp(GenData(Type_of_Problem),"Uniaxial")==0)
model BasicBuilder -ndm 1 -ndf 1
*elseif(strcmp(GenData(Type_of_Problem),"2D-Frame")==0)
model BasicBuilder -ndm 2 -ndf 3
*elseif(strcmp(GenData(Type_of_Problem),"PlaneStress2D")==0)
model BasicBuilder -ndm 2 -ndf 2
*elseif(strcmp(GenData(Type_of_Problem),"PlaneStrain2D")==0)
model BasicBuilder -ndm 2 -ndf 2
*elseif(strcmp(GenData(Type_of_Problem),"3D-Frame")==0)
model BasicBuilder -ndm 3 -ndf 6
*elseif(strcmp(GenData(Type_of_Problem),"Solids")==0)
model BasicBuilder -ndm 3 -ndf 6
*endif
# ------------------------------
# source files (library)
source RCcircSection.tcl
source MomentCurvature.tcl
source RCcircwallSection.tcl
source RCsection.tcl
source Units&Constants.tcl
# ------------------------------
# Create nodes & add to Domain - command: node nodeId ($coord)
*loop nodes
*format "%8i %10.3f %10.3f %10.3f"
node *NodesNum *NodesCoord(1) *NodesCoord(2) *NodesCoord(3)
*end nodes
# ------------------------------
# Create masses at nodes - command: mass nodeId (ndf $mass)
*Set Cond mass
*loop nodes *OnlyInCond
*format "%8i %10.1f %10.1f %10.1f %10.2f %10.2f %10.2f"
mass *NodesNum *cond(1) *cond(2) *cond(3) *cond(4) *cond(5) *cond(6)
*end nodes
# ------------------------------
# Nodal Constraints - command: fix nodeId (ndf $constr)
*Set Cond Point-Constraints
*loop nodes *OnlyInCond
*format "%8i %8i %8i %8i %8i %8i %8i"
fix *NodesNum *cond(1) *cond(2) *cond(3) *cond(4) *cond(5) *cond(6)
*end nodes
# ------------------------------
# Multipoint Constraints
# 1) equalDOF - command: equalDOF $master $slave ($dof)
*Set Cond equalDOF
*loop nodes *OnlyInCond
*if(strcmp(cond(1),"Master")==0)*\
*\equalDOF *NodesNum *\
*loop nodes *OnlyInCond
*if(strcmp(cond(1),"Slave")==0)*\
*Format "%8i %8i %8i %8i %8i %8i %8i"
*\ *NodesNum *cond(2) *cond(3) *cond(4) *cond(5) *cond(6) *cond(7)
*endif
*end nodes
*endif
*end nodes
# 2) rigidDiaphragm - command: rigidDiaphragm $perpDirn $masternode
($slavenodes)
*Set Cond rigidDiaphragm *OnlyInCond
*if(strcmp(cond(1),"XY")==0)
rigidDiaphragm 3 *\
*elseif(strcmp(cond(1),"XZ")==0)
rigidDiaphragm 2 *\
*elseif(strcmp(cond(1),"YZ")==0)
rigidDiaphragm 1 *\
*endif
*loop nodes *OnlyInCond
*if(strcmp(cond(2),"Master")==0)
*Nodesnum *\
*loop nodes *OnlyInCond
*if(strcmp(cond(2),"Slave")==0)
*NodesNum *\
*endif
*end nodes
*endif
*end nodes
# 3) rigidLink- command: rigidLink $type(rod,beam) $master $slave
*Set Cond rigidLink *OnlyInCond
*if(strcmp(cond(1),"rod")==0)*\
rigidLink rod *\
*elseif(strcmp(cond(1),"beam")==0)*\
rigidLink beam *\
*endif
*loop nodes *OnlyInCond
*if(strcmp(cond(2),"Master")==0)
*NodesNum *\
*loop nodes *OnlyInCond
*if(strcmp(cond(2),"Slave")==0)
*NodesNum
*endif
*end nodes
*endif
*end nodes
# ------------------------------
# Materials
# uniAxial Materials
# 1) Elastic -Command: uniaxialMaterial Elastic $tag $E $damping
*loop materials
*If(MatProp(consider_uniElastic,Int)!=0)*\
uniaxialMaterial Elastic *MatNum *MatProp(uni_E) *MatProp(uni_damping)
*endif
*End materials
# 2) Elastic-Perfectly Plastic
*loop materials
*If(MatProp(consider_uniElasticPP,Int)!=0)*\
uniaxialMaterial ElasticPP *MatNum *MatProp(PP_E)
*MatProp(PP_epsyP)*MatProp(PP_epsyN) *MatProp(PP_epsyO)
*endif
*End materials
# 3) Elastic-Perfectly Plastic GAP tension
*loop materials
*If(MatProp(consider_tensionGAP,Int)!=0)*\
uniaxialMaterial ElasticPPGap *MatNum *MatProp(gap_E) *\
*MatProp(gap_Fy) *MatProp(initial_gap)
*endif
*End materials
# 4) Elastic-Perfectly Plastic GAP compression
*loop materials
*If(MatProp(consider_compGAP,Int)!=0)
uniaxialMaterial ElasticPPGap *MatNum *MatProp(gap_Ecomp) *\
*MatProp(gap_Fycomp) *MatProp(initial_gapcomp)
*endif
*End materials
# 5) Hardening
*loop materials
*If(MatProp(consider_HardeningMaterial,Int)!=0)
uniaxialMaterial Hardening *MatNum *MatProp(Hard_E) *\
*MatProp(Hard_Fy) *MatProp(Iso_Hard_Mod) *MatProp(Kin_Hard_Mod)
*MatProp(visco_plastic_coef)
*endif
*End materials
# 6) Elastic_NoTension
*loop materials
*If(MatProp(consider_Elastic_NoTension,Int)!=0)
uniaxialMaterial ENT *MatNum *MatProp(ENT_E)
*endif
*End materials
# 7) HystereticMat
*loop materials
*If(MatProp(consider_HystereticMat,Int)!=0)
uniaxialMaterial Hysteretic *MatNum *MatProp(HM_stress1p) *\
*MatProp(HM_stress1p) *MatProp(HM_strain1p) *MatProp(HM_stress2p)
*MatProp(HM_strain2p) *\
*MatProp(HM_stress3p) *MatProp(HM_strain3p) *\
*MatProp(HM_stress1n) *MatProp(HM_strain1n) *MatProp(HM_stress2n)
*MatProp(HM_strain2n) *\
*MatProp(HM_stress3n) *MatProp(HM_strain3n) *MatProp(HM_pinchstrain)
*MatProp(HM_pinchstrain)*\
*MatProp(HM_pinchstress) *MatProp(HM_ductdamage)
*MatProp(HM_energydamage) *MatProp(HM_degradedunlstiff)
*endif
*End materials
# 8) ViscousMat
*loop materials
*If(MatProp(consider_ViscousMat,Int)!=0)
uniaxialMaterial Viscous *MatNum *MatProp(VM_tangent)
*MatProp(VM_damping)
*endif
*End materials
# 9) STEEL
# 9a) Steel01
*loop materials
*If(MatProp(consider_Steel01,Int)!=0)
uniaxialMaterial Steel01 *MatNum *MatProp(Steel01_Fy)
*MatProp(Steel01_Eo) *\
*MatProp(Steel01_hard_ratio) *MatProp(Steel01_hard_ratio)
*MatProp(Steel01_a1) *\
*MatProp(Steel01_a2) *MatProp(Steel01_a3) *MatProp(Steel01_a4)
*endif
*End materials
# 9b) Steel02
*loop materials
*If(MatProp(consider_Steel02,Int)!=0)
uniaxialMaterial Steel02 *MatNum *MatProp(Steel02_Fy)
*MatProp(Steel02_Eo) *\
*MatProp(Steel02_hard_ratio) *MatProp(Steel02_R0) *MatProp(Steel02_cR1) *\
*MatProp(Steel02_cR2) *MatProp(Steel01_a1) *MatProp(Steel01_a2)
*MatProp(Steel01_a3) *\
*MatProp(Steel01_a4)
*endif
*End materials
# 10) CONCRETE
# 10a) Concrete01 (compression curve)
*loop materials
*If(MatProp(consider_Concrete01,Int)!=0)
uniaxialMaterial Concrete01 *MatNum *MatProp(Concrete01_Fpc)
*MatProp(Concrete01_epsc0) *\
*MatProp(Concrete01_Fpcu) *MatProp(Concrete01_epscu)
*endif
*End materials
# 10b) Concrete02 (compression With linear tension softening)
*loop materials
*If(MatProp(consider_Concrete02,Int)!=0)
uniaxialMaterial Concrete02 *MatNum *MatProp(Concrete02_Fpc)
*MatProp(Concrete02_epsc0) *\
*MatProp(Concrete02_Fpcu) *MatProp(Concrete02_epscu)
*MatProp(Concrete02_lambda) *\
*MatProp(Concrete02_ft) *MatProp(Concrete02_Ets_linear)
*endif
*End materials
# 10c) Concrete03 (compression With nonlinear tension softening)
*loop materials
*If(MatProp(consider_Concrete03,Int)!=0)
uniaxialMaterial Concrete03 *MatNum *MatProp(Concrete03_Fpc)
*MatProp(Concrete03_epsc0) *\
*MatProp(Concrete03_Fpcu) *MatProp(Concrete03_epscu)
*MatProp(Concrete03_lambda) *\
*MatProp(Concrete03_ft) *MatProp(Concrete03_epsto)
*MatProp(Concrete03_fto) *\
*MatProp(Concrete03_beta) *MatProp(Concrete03_eptsu)
*endif
*End materials
# Frame Sections:
# 1) Elastic -command: Elastic $secTag $E $A $Iz $Iy $G $J
*loop materials
*If(MatProp(consider_elastic,Int)!=0)
section Elastic *MatNum *MatProp(Elastic_E) *\
*MatProp(Elastic_Area) *\
*MatProp(Elastic_Iz) *\
*MatProp(Elastic_Iy) *\
*MatProp(Elastic_G) *\
*MatProp(Elastic_J)
*endif
*End materials
# 2)proc RCsection {id h b cover coreID coverID steelID numBars
# barArea nfCoreY nfCoreZ nfCoverY nfCoverZ}
*loop materials
*If(MatProp(consider_Rect),Int)==1)
RCsection *\
*MatNum *MatProp(Rect_Height) *\
*MatProp(Rect_Width) *\
*MatProp(Rect_cover) *\
1 1 1 *\
*MatProp(Rect_NBarSide) *\
*MatProp(Rect_Ab) *\
15 15 15 1
*endif
*End materials
# 3)proc RCcircSection {id ri ro cover coreID coverID steelID
# numBars barArea nfCoreR nfCoreT nfCoverR nfCoverT}
*loop materials
*If(MatProp(consider_Circ),Int)==1)
RCcircSectio *\
*MatNum 0.0 *MatProp(Circ_radius) *\
*MatProp(Circ_cover) *\
1 1 1 *\
*MatProp(Circt_NBars) *\
*MatProp(Circ_Ab) *\
15 15 1 15
*endif
*End materials
# 4)proc RCcircwallSection {id ri ro cover coreID coverID steelID check!
# numBars barArea nfCoreR nfCoreT nfCoverR nfCoverT}
*loop materials
*If(MatProp(consider_Circwall),Int)==1)
proc RCcircwallSection {
*MatNum *MatProp(Wall_ri) *\
*MatProp(Wall_ro)
*MatProp(Wall_cover) *\
1 1 1 *\
*MatProp(Wall_NBars) *\
*MatProp(Wall_Ab) *\
20 36 1 36
}
*endif
*End materials
# more materials here!
# ------------------------------
# Elements
*Set cond Truss
*loop elems *OnlyInCond
*If(cond(consider_TrussArea,Int)==1)
*Format "%5i %5i %5i %6.1f %4i"
element truss *elemsnum *ElemsConec *cond(TrussArea) *elemsmat
*Else
*Format "%5i %5i %5i %5i"
element truss *elemsnum *ElemsConec *elemsmat
*endif
*end elems
----------------------------------------------------------------------------
----
BOOK: GeneralConstraints
NUMBER: 1 CONDITION:Point-Constraints
CONDTYPE: over points
CONDMESHTYPE: over nodes
QUESTION:X#CB#(1,0)
VALUE:0
QUESTION:Y#CB#(1,0)
VALUE:0
QUESTION:Z#CB#(1,0)
VALUE:0
QUESTION:ROT-X#CB#(1,0)
VALUE:0
QUESTION:ROT-Y#CB#(1,0)
VALUE:0
QUESTION:ROT-Z#CB#(1,0)
VALUE:0
END CONDITION
NUMBER: 2 CONDITION:Line-Constraints
CONDTYPE: over lines
CONDMESHTYPE: over nodes
QUESTION:X-Constraint#CB#(1,0)
VALUE: 1
QUESTION:Y-Constraint#CB#(1,0)
VALUE: 1
QUESTION:Z-Constraint#CB#(1,0)
VALUE: 1
END CONDITION
NUMBER: 3 CONDITION: Point-Force-Load
CONDTYPE: over points
CONDMESHTYPE: over nodes
QUESTION:X-Force
VALUE: 0.0
QUESTION:Y-Force
VALUE: 0.0
QUESTION:Z-Force
VALUE: 0.0
QUESTION:X-Moment
VALUE: 0.0
QUESTION:Y-Moment
VALUE: 0.0
QUESTION:Z-Moment
VALUE: 0.0
END CONDITION
NUMBER: 4 CONDITION:mass
CONDTYPE: over points
CONDMESHTYPE: over nodes
QUESTION:X
VALUE:0.0
QUESTION:Y
VALUE: 0.0
QUESTION:Z
VALUE: 0.0
QUESTION:ROT-X
VALUE:0.0
QUESTION:ROT-Y
VALUE: 0.0
QUESTION:ROT-Z
VALUE: 0.0
END CONDITION
NUMBER: 5 CONDITION:rigidDiaphragm
CONDTYPE: over points
CONDMESHTYPE: over nodes
QUESTION:Plane#CB#(none,XY,XZ,YZ)
VALUE:none
QUESTION:rigid#CB#(Master,Slave)
VALUE: Master
END CONDITION
NUMBER: 6 CONDITION: equalDOF
CONDTYPE: over points
CONDMESHTYPE: over nodes
QUESTION: equalDOF:#CB#(Master,Slave)
VALUE: Master
QUESTION:X#CB#(1,0)
VALUE:1
QUESTION:Y#CB#(1,0)
VALUE: 1
QUESTION:Z#CB#(1,0)
VALUE: 0
QUESTION:ROT-X#CB#(1,0)
VALUE:0
QUESTION:ROT-Y#CB#(1,0)
VALUE: 0
QUESTION:ROT-Z#CB#(1,0)
VALUE: 0
END CONDITION
NUMBER: 7 CONDITION:rigidLink
CONDTYPE: over points
CONDMESHTYPE: over nodes
QUESTION:TypeLink#CB#(none,rod,beam)
VALUE:none
QUESTION:Link:#CB#(Master,Slave)
VALUE: Master
END CONDITION
NUMBER: 8 CONDITION: Line-Load
CONDTYPE: over lines
CONDMESHTYPE: over elems
QUESTION:Normal-Presure:
VALUE: 0.0
END CONDITION
BOOK: Frame Properties
NUMBER: 9 CONDITION: Truss
CONDTYPE: over lines
CONDMESHTYPE: over elems
QUESTION:consider_TrussArea#CB#(1,0)
VALUE:0
QUESTION:TrussArea
VALUE:500
END CONDITION
NUMBER: 10 CONDITION: nonlinearBeamColumn
CONDTYPE: over lines
CONDMESHTYPE: over elems
QUESTION:consider_NLBC#CB#(0,1)
VALUE:0
QUESTION:NLBC_numIntPoints:
VALUE:5
QUESTION:NLBC_mass(kg/m):
VALUE:100
QUESTION:NLBC_maxIter:
VALUE:1
QUESTION:NLBC_tol:
VALUE:10E-16
END CONDITION
NUMBER: 11 CONDITION: beamWithHinges
CONDTYPE: over lines
CONDMESHTYPE: over elems
QUESTION:consider_bWH#CB#(0,1)
VALUE:0
QUESTION:bWH_HingeLi:
VALUE:500
QUESTION:bWH_HingeLj:
VALUE:500
QUESTION:bWH_mass(kg/m):
VALUE:100
QUESTION:bWH_maxIter:
VALUE:1
QUESTION:bWH_tol:
VALUE:10E-16
END CONDITION
NUMBER: 12 CONDITION: dispBeamColumn
CONDTYPE: over lines
CONDMESHTYPE: over elems
QUESTION:consider_dBC#CB#(0,1)
VALUE:0
QUESTION:dBC_numIntPoints:
VALUE:5
QUESTION:dBC_mass(kg/m):
VALUE:100
END CONDITION
BOOK: FE Properties
NUMBER: 13 CONDITION: Quad
CONDTYPE: over surfaces
CONDMESHTYPE: over elems
QUESTION:consider_Quad#CB#(0,1)
VALUE:0
QUESTION:Quad_thickness:
VALUE:250
QUESTION:Quad_pressure:
VALUE:0
QUESTION:Quad_density(kg/m3):
VALUE:2400
QUESTION:Quad_bodyforce1:
VALUE:0
QUESTION:Quad_bodyforce2:
VALUE:0
END CONDITION
NUMBER: 14 CONDITION: 8nodeBrick
CONDTYPE: over volumes
CONDMESHTYPE: over elems
QUESTION:consider_8nodeBrick#CB#(0,1)
VALUE:0
QUESTION:8nodeBrick_density(kg/m3)
VALUE:2400
QUESTION:8nodeBrick_bodyforce1:
VALUE:0
QUESTION:8nodeBrick_bodyforce2:
VALUE:0
QUESTION:8nodeBrick_bodyforce3:
VALUE:0
END CONDITION
----------------------------------------------------------------------------
----
PROBLEM DATA
BOOK: ModelBuilder
QUESTION: Title
VALUE: Default_Title
QUESTION:
Type_of_Problem:#CB#(Uniaxial,2D-Frame,PlaneStress2D,PlaneStrain2D,3D-Frame,
Solids)
VALUE: 2D-Frame
BOOK: AnalysisGeneral
TITLE: Numberer
QUESTION: Numberer:#CB#(Plain,RCM)
VALUE: RCM
TITLE: Analysis
QUESTION: Analysis:#CB#(Static,Transient,VariableTransient)
VALUE: Static
TITLE: Eigen
QUESTION: Type_eigen#cb#(frequency,generalized,standard)
VALUE: standard
QUESTION: NumberEig
VALUE: 1
TITLE: Execution
QUESTION:
Solver:#CB#(BandSPD,BandGeneral,ProfileSPD,UmfPack,SparseSPD,SparseGeneral)
VALUE: BandSPD
QUESTION: LoadSteps
VALUE: 1
QUESTION: Increment
VALUE: 0.1
QUESTION: MinIncr
VALUE: 0.0
QUESTION: MaxIncr
VALUE: 0.0
QUESTION: NumberIterations
VALUE: 0
TITLE: ConvergenceTest
QUESTION: ConvergenceTest:#CB#(NormUnb,NormDispl,EnergyInc)
VALUE: NormUnb
QUESTION: Tolerance
VALUE: 0.0001
QUESTION: maxNumIter
VALUE: 40
QUESTION:
PrintOption#CB#(NoPrint,PrintEachStep,PrintwhenConverge,PrintNormdUdR,PrintE
rrorandContinueAnal)
VALUE: NoPrint
BOOK: AnalysisConstraints
TITLE: Plain
QUESTION: Plain#CB#(1,0)
VALUE: 1
TITLE: Lagrange
QUESTION: Lagrange#CB#(1,0)
VALUE: 0
QUESTION: LagSinglePointFactor
VALUE: 1
QUESTION: LagMultiplePointFactor
VALUE: 1
TITLE: Penalty
QUESTION: Penalty#CB#(1,0)
VALUE: 0
QUESTION: PenSinglePointFactor
VALUE: 100000
QUESTION: PenMultiplePointFactor
VALUE: 100000
TITLE: Transformation
QUESTION: Transformation#CB#(1,0)
VALUE: 0
BOOK: AnalysisAlgorithm
QUESTION: Linear#CB#(1,0)
VALUE: 1
QUESTION: Newton#CB#(1,0)
VALUE: 0
QUESTION: NewtonLineSearch#CB#(1,0)
VALUE: 0
QUESTION: ratio
VALUE: 0.5~0.8
QUESTION: ModNewton#CB#(1,0)
VALUE: 0
QUESTION: KrylovNewton#CB#(1,0)
VALUE: 0
QUESTION: BFGS#CB#(1,0)
VALUE: 0
QUESTION: Broyden#CB#(1,0)
VALUE: 0
QUESTION: numberIterWithinTimeStep
VALUE: 40
BOOK: AnalysisIntegrator
TITLE: LoadControl
QUESTION: LCFirstLoadInc#CB#(1,0)
VALUE: 1
QUESTION: LCFirstLoadInc
VALUE: 1
QUESTION: LCFactorLoadInc
VALUE: 1
QUESTION: LCMinLoadInc
VALUE: 1
QUESTION: LCMaxLoadInc
VALUE: 1
TITLE: DisplControl
QUESTION: DisplControl#CB#(1,0)
VALUE: 0
QUESTION: ControlNode
VALUE: 0
QUESTION: DoF-X#CB#(1,0)
VALUE: 1
QUESTION: DoF-Y#CB#(1,0)
VALUE: 0
QUESTION: DoF-Z#CB#(1,0)
VALUE: 0
QUESTION: DoF-rotX#CB#(1,0)
VALUE: 0
QUESTION: DoF-rotY#CB#(1,0)
VALUE: 0
QUESTION: DoF-rotZ#CB#(1,0)
VALUE: 0
QUESTION: DCFirstDisplInc
VALUE: 1
QUESTION: DCFactorDisplInc
VALUE: 1
QUESTION: DCMinDisplInc
VALUE: 1
QUESTION: DCMaxDisplInc
VALUE: 1
TITLE: MinUnbDispl
QUESTION: MinUnbDispl#CB#(1,0)
VALUE: 0
QUESTION: MUDFirstLoadInc
VALUE: 1
QUESTION: MUDFactorLoadInc
VALUE: 1
QUESTION: MUDMinLoadInc
VALUE: 1
QUESTION: MUDMaxLoadInc
VALUE: 1
TITLE: ArcLength
QUESTION: ArcLength#CB#(1,0)
VALUE: 0
QUESTION: ArcLength
VALUE: 1
QUESTION: Alpha
VALUE: 30??
TITLE: Newmark
QUESTION: Newmark#CB#(1,0)
VALUE: 0
QUESTION: Newmgamma
VALUE: 0.5
QUESTION: Newmbeta
VALUE: 0.25
QUESTION: NewmalphaM
VALUE: 0.0
QUESTION: NewmbetaK
VALUE: 0.0
QUESTION: NewmbetaKinit
VALUE: 0.0
QUESTION: NewmbetaKcomm
VALUE: 0.0
TITLE: Hilbert-Hughes-Taylor
QUESTION: HHT#CB#(1,0)
VALUE: 0
QUESTION: HHTgamma
VALUE: 0.5
QUESTION: HHTalphaM
VALUE: 0.0
QUESTION: HHTbetaK
VALUE: 0.0
QUESTION: HHTbetaKinit
VALUE: 0.0
QUESTION: HHTbetaKcomm
VALUE: 0.0
END GENERAL DATA