*Heading
 A one element truss along global x-axis modeled using T3D2 element and 
 temperature dependence of Young's modulus
 Reference solution for vuel_truss_3d_1el_temp.inp
*Parameter
 CsArea=1.002
 YoungsMod1=2.1E7
 temp1=25.0
 YoungsMod2=2.1E6
 temp2=100.0 
 PoissonRatio=0.0
 Density=7200.0
*Node
 1, 0.0, 0.0, 0.0
 2, 1.0, 0.0, 0.0
*Nset, Nset=AllNodes
 1,2
*Nset, Nset=LeftNode
 1,
*nset, nset=qa_test_leftnode
 1,
*Nset, Nset=RightNode
 2,
*nset, nset=qa_test_rightnode
 2,
*Element, Type=T3D2, Elset=AllElements
 1, 1, 2
*elset, elset=qa_test_allEl
 1,
*Material, Name=Mat1
*Density
 <Density>,
*Elastic
 <YoungsMod1>,<PoissonRatio>,<temp1>
 <YoungsMod2>,<PoissonRatio>,<temp2>
*Solid Section, Elset=AllElements, Material=Mat1
 1.0,
*Boundary
 LeftNode, 1, 3, 0.0
 RightNode, 2, 3, 0.0
*Amplitude, name=LoadAmp, Definition=Smooth Step
 0.0, 0.0, 1.0, 1.0
*Initial Conditions, type=temperature
 AllNodes, 25.0
****************************************
*Step, Nlgeom=Yes
*Dynamic, Explicit, Element
 ,1.0
*Bulk Viscosity
 0,0, 0.0
*Cload, Amplitude=LoadAmp
 RightNode, 1, 1.0e6
*Temperature
 AllNodes, 100.0
*Output, Field, Var=Preselect
*Output, History, Freq=1
*Node Output, Nset=AllNodes
 U1, V1, A1, RF1
*node output, nset=qa_test_leftnode
 RF1,
*node output, nset=qa_test_rightnode
 u1,
*element output, elset=qa_test_allEl
 FV1,
*Energy Output
*End Step