*Heading ** Job name: FR-Auslenkung Model name: FR-Auslenkung ** Generated by: Abaqus/CAE 6.12-1 *Preprint, echo=NO, model=NO, history=NO, contact=NO ** ** PARTS ** *Part, name=Einspannung *Node 1, 0., 20., 0. *Nset, nset=Einspannung-RefPt_, internal 1, *End Part ** *Part, name="Masse 1" *Node 1, 0., 0., 0. *Nset, nset="Masse 1-RefPt_", internal 1, *End Part ** *Part, name="Masse 2" *Node 1, 0., 10., 0. *Nset, nset="Masse 2-RefPt_", internal 1, *End Part ** ** ** ASSEMBLY ** *Assembly, name=Assembly ** *Instance, name=Einspannung-1, part=Einspannung *End Instance ** *Instance, name="Masse 1-1", part="Masse 1" *End Instance ** *Instance, name="Masse 2-1", part="Masse 2" *End Instance ** *Nset, nset=Set-2, instance="Masse 2-1" 1, *Nset, nset=Set-7, instance=Einspannung-1 1, *Nset, nset=Set-8, instance="Masse 2-1" 1, *Nset, nset=Set-9, instance="Masse 1-1" 1, *Nset, nset=Set-10, instance="Masse 1-1" 1, *Nset, nset=ALL, instance=Einspannung-1 1, *Nset, nset=ALL, instance="Masse 1-1" 1, *Nset, nset=ALL, instance="Masse 2-1" 1, *Nset, nset=Set-12, instance="Masse 1-1" 1, *Nset, nset=Set-1, instance="Masse 1-1" 1, *Nset, nset="Masse 1", instance="Masse 1-1" 1, *Nset, nset=Masse2, instance="Masse 2-1" 1, *Nset, nset=Fix-oben, instance=Einspannung-1 1, *Element, type=MASS, elset="Set-1_Masse 1_" 1, "Masse 1-1".1 *Mass, elset="Set-1_Masse 1_" 1., *Element, type=MASS, elset="Set-2_Masse 2_" 2, "Masse 2-1".1 *Mass, elset="Set-2_Masse 2_" 5., *Spring, elset="Feder 1-spring" 100. *Element, type=SpringA, elset="Feder 1-spring" 3, "Masse 2-1".1, "Masse 1-1".1 *Spring, elset="Feder 2-spring" 500. *Element, type=SpringA, elset="Feder 2-spring" 4, Einspannung-1.1, "Masse 2-1".1 *End Assembly *Amplitude, name=Amplitude 0., 1., 20., 1. ** ** BOUNDARY CONDITIONS ** ** Name: BC-m2-mitte Type: Displacement/Rotation *Boundary Set-8, 1, 1 Set-8, 6, 6 ** Name: Einspannung-oben Type: Symmetry/Antisymmetry/Encastre *Boundary Set-7, ENCASTRE ** ---------------------------------------------------------------- ** ** STEP: Modenbestimmung ** *Step, name=Modenbestimmung, perturbation Berechnung der Moden *Frequency, eigensolver=Lanczos, acoustic coupling=on, normalization=displacement 5, , , , , ** ** BOUNDARY CONDITIONS ** ** Name: SB-m1-unten Type: Secondary base *Boundary, base name=SB-m1-unten "Masse 1", 1, 1 "Masse 1", 2, 2 "Masse 1", 3, 3 "Masse 1", 4, 4 "Masse 1", 5, 5 "Masse 1", 6, 6 ** ** OUTPUT REQUESTS ** *Restart, write, frequency=0 ** ** FIELD OUTPUT: F-Output-1 ** *Output, field, variable=PRESELECT *End Step ** ---------------------------------------------------------------- ** ** STEP: Frequency Response ** *Step, name="Frequency Response", perturbation Frequency Response 0-20 Hz in 50 Schritten *Steady State Dynamics 0., 20., 50, 3. *Modal Damping 1, 5, 0.01 ** ** BOUNDARY CONDITIONS ** ** Name: Base Motion-m1 Type: Displacement base motion *Base Motion, type=DISPLACEMENT, dof=2, base name=SB-m1-unten, amplitude=Amplitude, scale=1. ** ** OUTPUT REQUESTS ** ** ** FIELD OUTPUT: F-Output-2 ** *Output, field, variable=PRESELECT ** ** HISTORY OUTPUT: H-Output-1 ** *Output, history *Node Output, nset=ALL RF1, RF2, RF3, U2 *End Step