Fig. 1 Il modello utilizzato
=============================================================================== STRAND6.15 | DATA LISTING - STRUCTURE INPUT =============================================================================== FILENAME : C:\STRAND61\MODELLI\CONTATTO HEADING : STRAND6.1 PROJECT : CREATED BY : STEFANO SECCHI REVISION : 1.0 DATE CREATED : 12 / 10 / 1995 DATE MODIFIED : 12 / 10 / 1995 NODE TOTAL = 114 NODE X Y Z 1 0.000000000000 0.000000000000 0.000000000000 2 100.000000000000 0.000000000000 0.000000000000 3 0.000000000000 100.000000000000 0.000000000000 4 100.000000000000 100.000000000000 0.000000000000 5 200.000000000000 0.000000000000 0.000000000000 6 200.000000000000 100.000000000000 0.000000000000 7 300.000000000000 0.000000000000 0.000000000000 8 300.000000000000 100.000000000000 0.000000000000 9 400.000000000000 0.000000000000 0.000000000000 10 400.000000000000 100.000000000000 0.000000000000 11 500.000000000000 0.000000000000 0.000000000000 12 500.000000000000 100.000000000000 0.000000000000 13 600.000000000000 0.000000000000 0.000000000000 14 600.000000000000 100.000000000000 0.000000000000 15 700.000000000000 0.000000000000 0.000000000000 16 700.000000000000 100.000000000000 0.000000000000 17 800.000000000000 0.000000000000 0.000000000000 18 800.000000000000 100.000000000000 0.000000000000 19 900.000000000000 0.000000000000 0.000000000000 20 900.000000000000 100.000000000000 0.000000000000 21 1000.000000000000 0.000000000000 0.000000000000 22 1000.000000000000 100.000000000000 0.000000000000 23 1100.000000000000 0.000000000000 0.000000000000 24 1100.000000000000 100.000000000000 0.000000000000 25 0.000000000000 200.000000000000 0.000000000000 26 100.000000000000 200.000000000000 0.000000000000 27 200.000000000000 200.000000000000 0.000000000000 28 300.000000000000 200.000000000000 0.000000000000 29 400.000000000000 200.000000000000 0.000000000000 30 500.000000000000 200.000000000000 0.000000000000 31 600.000000000000 200.000000000000 0.000000000000 32 700.000000000000 200.000000000000 0.000000000000 33 800.000000000000 200.000000000000 0.000000000000 34 900.000000000000 200.000000000000 0.000000000000 35 1000.000000000000 200.000000000000 0.000000000000 36 1100.000000000000 200.000000000000 0.000000000000 37 0.000000000000 300.000000000000 0.000000000000 38 100.000000000000 300.000000000000 0.000000000000 39 200.000000000000 300.000000000000 0.000000000000 40 300.000000000000 300.000000000000 0.000000000000 41 400.000000000000 300.000000000000 0.000000000000 42 500.000000000000 300.000000000000 0.000000000000 43 600.000000000000 300.000000000000 0.000000000000 44 700.000000000000 300.000000000000 0.000000000000 45 800.000000000000 300.000000000000 0.000000000000 46 900.000000000000 300.000000000000 0.000000000000 47 1000.000000000000 300.000000000000 0.000000000000 48 1100.000000000000 300.000000000000 0.000000000000 49 0.000000000000 400.000000000000 0.000000000000 50 100.000000000000 400.000000000000 0.000000000000 51 200.000000000000 400.000000000000 0.000000000000 52 300.000000000000 400.000000000000 0.000000000000 53 400.000000000000 400.000000000000 0.000000000000 54 500.000000000000 400.000000000000 0.000000000000 55 600.000000000000 400.000000000000 0.000000000000 56 700.000000000000 400.000000000000 0.000000000000 57 800.000000000000 400.000000000000 0.000000000000 58 900.000000000000 400.000000000000 0.000000000000 59 1000.000000000000 400.000000000000 0.000000000000 60 1100.000000000000 400.000000000000 0.000000000000 61 0.000000000000 500.000000000000 0.000000000000 62 100.000000000000 500.000000000000 0.000000000000 63 200.000000000000 500.000000000000 0.000000000000 64 300.000000000000 500.000000000000 0.000000000000 65 400.000000000000 500.000000000000 0.000000000000 66 500.000000000000 500.000000000000 0.000000000000 67 600.000000000000 500.000000000000 0.000000000000 68 700.000000000000 500.000000000000 0.000000000000 69 800.000000000000 500.000000000000 0.000000000000 70 900.000000000000 500.000000000000 0.000000000000 71 1000.000000000000 500.000000000000 0.000000000000 72 1100.000000000000 500.000000000000 0.000000000000 73 0.000000000000 600.000000000000 0.000000000000 74 100.000000000000 600.000000000000 0.000000000000 75 200.000000000000 600.000000000000 0.000000000000 76 300.000000000000 600.000000000000 0.000000000000 77 400.000000000000 600.000000000000 0.000000000000 78 500.000000000000 600.000000000000 0.000000000000 79 600.000000000000 600.000000000000 0.000000000000 80 700.000000000000 600.000000000000 0.000000000000 81 800.000000000000 600.000000000000 0.000000000000 82 900.000000000000 600.000000000000 0.000000000000 83 1000.000000000000 600.000000000000 0.000000000000 84 1100.000000000000 600.000000000000 0.000000000000 85 0.000000000000 650.000000000000 0.000000000000 86 100.000000000000 650.000000000000 0.000000000000 87 200.000000000000 650.000000000000 0.000000000000 88 300.000000000000 650.000000000000 0.000000000000 89 400.000000000000 650.000000000000 0.000000000000 90 500.000000000000 650.000000000000 0.000000000000 91 600.000000000000 650.000000000000 0.000000000000 92 700.000000000000 650.000000000000 0.000000000000 93 800.000000000000 650.000000000000 0.000000000000 94 900.000000000000 650.000000000000 0.000000000000 95 1000.000000000000 650.000000000000 0.000000000000 96 1100.000000000000 650.000000000000 0.000000000000 97 0.000000000000 700.000000000000 0.000000000000 98 100.000000000000 700.000000000000 0.000000000000 99 200.000000000000 700.000000000000 0.000000000000 100 300.000000000000 700.000000000000 0.000000000000 101 400.000000000000 700.000000000000 0.000000000000 102 500.000000000000 700.000000000000 0.000000000000 103 600.000000000000 700.000000000000 0.000000000000 104 700.000000000000 700.000000000000 0.000000000000 105 800.000000000000 700.000000000000 0.000000000000 106 900.000000000000 700.000000000000 0.000000000000 107 1000.000000000000 700.000000000000 0.000000000000 108 1100.000000000000 700.000000000000 0.000000000000 109 300.000000000000 -350.000000000000 0.000000000000 110 400.000000000000 -350.000000000000 0.000000000000 111 500.000000000000 -350.000000000000 0.000000000000 112 600.000000000000 -350.000000000000 0.000000000000 113 700.000000000000 -350.000000000000 0.000000000000 114 800.000000000000 -350.000000000000 0.000000000000 FREEDOM CONDITIONS FOR NODES : (0 -> FREE ; 1 -> FIXED) DEFAULT : 0 0 1 1 1 0 NODE DX DY DZ RX RY RZ 1 1 1 1 1 1 1 2 1 1 1 1 1 1 5 1 1 1 1 1 1 7 1 1 1 1 1 1 9 1 1 1 1 1 1 11 1 1 1 1 1 1 13 1 1 1 1 1 1 15 1 1 1 1 1 1 17 1 1 1 1 1 1 19 1 1 1 1 1 1 21 1 1 1 1 1 1 23 1 1 1 1 1 1 REFERENCE TEMPERATURE = 0.0000E+00 TEMPERATURE DATA (NODAL) NODE TEMPERATURE 88 -1.0000E+00 89 -1.0000E+00 90 -1.0000E+00 91 -1.0000E+00 92 -1.0000E+00 93 -1.0000E+00 109 -1.0000E+00 110 -1.0000E+00 111 -1.0000E+00 112 -1.0000E+00 113 -1.0000E+00 114 -1.0000E+00 CONSTRAINT EQUATIONS TOTAL = 12 Eq.No. DOF N(i) A DOF N(j) B DOF N(k) C 1 DX( 109) = + 1.00000*DX( 88) + 0.00000 2 DY( 109) = + 1.00000*DY( 76) + 0.00000 3 DX( 110) = + 1.00000*DX( 89) + 0.00000 4 DY( 110) = + 1.00000*DY( 77) + 0.00000 5 DX( 111) = + 1.00000*DX( 90) + 0.00000 6 DY( 111) = + 1.00000*DY( 78) + 0.00000 7 DX( 112) = + 1.00000*DX( 91) + 0.00000 8 DY( 112) = + 1.00000*DY( 79) + 0.00000 9 DX( 113) = + 1.00000*DX( 92) + 0.00000 10 DY( 113) = + 1.00000*DY( 80) + 0.00000 11 DX( 114) = + 1.00000*DX( 93) + 0.00000 12 DY( 114) = + 1.00000*DY( 81) + 0.00000 BEAM TOTAL = 6 BEAM N1 N2 Nref Prop EndRel 1 88 109 0 1 1 1 1 1 1 1 2 89 110 0 1 1 1 1 1 1 1 3 90 111 0 1 1 1 1 1 1 1 4 91 112 0 1 1 1 1 1 1 1 5 92 113 0 1 1 1 1 1 1 1 6 93 114 0 1 1 1 1 1 1 1 PLATE TOTAL = 81 PLATE N1 N2 N3 N4 N5 N6 N7 N8 Prop Type 1 1 2 4 3 0 0 0 0 1 QUAD4 2 2 5 6 4 0 0 0 0 1 QUAD4 3 5 7 8 6 0 0 0 0 1 QUAD4 4 7 9 10 8 0 0 0 0 1 QUAD4 5 9 11 12 10 0 0 0 0 1 QUAD4 6 11 13 14 12 0 0 0 0 1 QUAD4 7 13 15 16 14 0 0 0 0 1 QUAD4 8 15 17 18 16 0 0 0 0 1 QUAD4 9 17 19 20 18 0 0 0 0 1 QUAD4 10 19 21 22 20 0 0 0 0 1 QUAD4 11 21 23 24 22 0 0 0 0 1 QUAD4 12 3 4 26 25 0 0 0 0 1 QUAD4 13 4 6 27 26 0 0 0 0 1 QUAD4 14 6 8 28 27 0 0 0 0 1 QUAD4 15 8 10 29 28 0 0 0 0 1 QUAD4 16 10 12 30 29 0 0 0 0 1 QUAD4 17 12 14 31 30 0 0 0 0 1 QUAD4 18 14 16 32 31 0 0 0 0 1 QUAD4 19 16 18 33 32 0 0 0 0 1 QUAD4 20 18 20 34 33 0 0 0 0 1 QUAD4 21 20 22 35 34 0 0 0 0 1 QUAD4 22 22 24 36 35 0 0 0 0 1 QUAD4 23 25 26 38 37 0 0 0 0 1 QUAD4 24 26 27 39 38 0 0 0 0 1 QUAD4 25 27 28 40 39 0 0 0 0 1 QUAD4 26 28 29 41 40 0 0 0 0 1 QUAD4 27 29 30 42 41 0 0 0 0 1 QUAD4 28 30 31 43 42 0 0 0 0 1 QUAD4 29 31 32 44 43 0 0 0 0 1 QUAD4 30 32 33 45 44 0 0 0 0 1 QUAD4 31 33 34 46 45 0 0 0 0 1 QUAD4 32 34 35 47 46 0 0 0 0 1 QUAD4 33 35 36 48 47 0 0 0 0 1 QUAD4 34 37 38 50 49 0 0 0 0 1 QUAD4 35 38 39 51 50 0 0 0 0 1 QUAD4 36 39 40 52 51 0 0 0 0 1 QUAD4 37 40 41 53 52 0 0 0 0 1 QUAD4 38 41 42 54 53 0 0 0 0 1 QUAD4 39 42 43 55 54 0 0 0 0 1 QUAD4 40 43 44 56 55 0 0 0 0 1 QUAD4 41 44 45 57 56 0 0 0 0 1 QUAD4 42 45 46 58 57 0 0 0 0 1 QUAD4 43 46 47 59 58 0 0 0 0 1 QUAD4 44 47 48 60 59 0 0 0 0 1 QUAD4 45 49 50 62 61 0 0 0 0 1 QUAD4 46 50 51 63 62 0 0 0 0 1 QUAD4 47 51 52 64 63 0 0 0 0 1 QUAD4 48 52 53 65 64 0 0 0 0 1 QUAD4 49 53 54 66 65 0 0 0 0 1 QUAD4 50 54 55 67 66 0 0 0 0 1 QUAD4 51 55 56 68 67 0 0 0 0 1 QUAD4 52 56 57 69 68 0 0 0 0 1 QUAD4 53 57 58 70 69 0 0 0 0 1 QUAD4 54 58 59 71 70 0 0 0 0 1 QUAD4 55 59 60 72 71 0 0 0 0 1 QUAD4 56 61 62 74 73 0 0 0 0 1 QUAD4 57 62 63 75 74 0 0 0 0 1 QUAD4 58 63 64 76 75 0 0 0 0 1 QUAD4 59 64 65 77 76 0 0 0 0 1 QUAD4 60 65 66 78 77 0 0 0 0 1 QUAD4 61 66 67 79 78 0 0 0 0 1 QUAD4 62 67 68 80 79 0 0 0 0 1 QUAD4 63 68 69 81 80 0 0 0 0 1 QUAD4 64 69 70 82 81 0 0 0 0 1 QUAD4 65 70 71 83 82 0 0 0 0 1 QUAD4 66 71 72 84 83 0 0 0 0 1 QUAD4 67 85 86 98 97 0 0 0 0 1 QUAD4 68 86 87 99 98 0 0 0 0 1 QUAD4 69 87 88 100 99 0 0 0 0 1 QUAD4 70 88 89 101 100 0 0 0 0 1 QUAD4 71 89 90 102 101 0 0 0 0 1 QUAD4 72 90 91 103 102 0 0 0 0 1 QUAD4 73 91 92 104 103 0 0 0 0 1 QUAD4 74 92 93 105 104 0 0 0 0 1 QUAD4 75 93 94 106 105 0 0 0 0 1 QUAD4 76 94 95 107 106 0 0 0 0 1 QUAD4 77 95 96 108 107 0 0 0 0 1 QUAD4 78 73 74 86 85 0 0 0 0 1 QUAD4 79 74 75 87 86 0 0 0 0 1 QUAD4 80 82 83 95 94 0 0 0 0 1 QUAD4 81 83 84 96 95 0 0 0 0 1 QUAD4 EDGE STRESS TOTAL = 81 LOAD CASE = 1 PLATE S1 S2 S3 S4 T1 T2 T3 T4 69 0.0000E+00 0.0000E+00 -2.0000E+03 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 70 0.0000E+00 0.0000E+00 -2.0000E+03 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 71 0.0000E+00 0.0000E+00 -2.0000E+03 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 72 0.0000E+00 0.0000E+00 -2.0000E+03 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 73 0.0000E+00 0.0000E+00 -2.0000E+03 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 74 0.0000E+00 0.0000E+00 -2.0000E+03 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 75 0.0000E+00 0.0000E+00 -2.0000E+03 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 BEAM PROPERTIES TOTAL = 2 TYPE = 1 Section Standard: Circular (OD= 3.568E+01 ID= 0.000E+00) Beam Type: Comp. Only CutoffType: ElastPlast Max.Comp.= 1.000E+11 E = 1.0000E+08 A = 1.0000E+03 J = 0.0000E+00 G = 0.0000E+00 I11 = 0.0000E+00 I22 = 0.0000E+00 Shear:L1 = 0.0000E+00 Shear:L2 = 0.0000E+00 NodLine:L1 = 0.0000E+00 NodLine:L2 = 0.0000E+00 UDL:1 = 0.0000E+00 UDL:2 = 0.0000E+00 TG:1 = 0.0000E+00 TG:2 = 0.0000E+00 Alpha = 5.0000E-02 SA11 = 0.0000E+00 Density = 0.0000E+00 SA22 = 0.0000E+00 Temperature Table = 0 BEAM PROPERTIES TOTAL = 2 TYPE = 2 Beam Type: Normal Beam E = 0.0000E+00 A = 0.0000E+00 J = 0.0000E+00 G = 0.0000E+00 I11 = 0.0000E+00 I22 = 0.0000E+00 Shear:L1 = 0.0000E+00 Shear:L2 = 0.0000E+00 NodLine:L1 = 0.0000E+00 NodLine:L2 = 0.0000E+00 UDL:1 = 0.0000E+00 UDL:2 = 0.0000E+00 TG:1 = 0.0000E+00 TG:2 = 0.0000E+00 Alpha = 0.0000E+00 SA11 = 0.0000E+00 Density = 0.0000E+00 SA22 = 0.0000E+00 Temperature Table = 0 PLATE PROPERTIES TOTAL = 1 TYPE = 1 ISOTROPIC Element : LinearQuad, PlateShell, Von Mises E = 3.0000E+05 Poisson Ratio = 4.0000E-01 Alpha = 0.0000E+00 Layers No. = 0 Memb.Thick = 1.0000E+01 Bend.Thick = 1.0000E+01 Pressure = 0.0000E+00 Density = 0.0000E+00 Stress:1 = 0.0000E+00 Stress:2 = 0.0000E+00 Stress:3 = 0.0000E+00 Stress:4 = 0.0000E+00 Shear :1 = 0.0000E+00 Shear :2 = 0.0000E+00 Shear :3 = 0.0000E+00 Shear :4 = 0.0000E+00 Temperature Table = 0 Stress-Strain Table = 0Risultati: E' stato utilizzato il solutore "Linear Static". Nella condizione di carico 1 devono essere inclusi anche gli effetti termici. Di seguito sono riportate una sequenza di immagini corrispondenti ad un carico crescente.
Fig. 2
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Fig. 6