kabete spiral

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Page: 1/15 Sheet: 1 Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4 STRUCTURAL ANALYSIS PROJECT KABETE SPIRAL STAIRCASE CLIENT CREATED BY Z X Y Isometric RFEM 5.01.0022 - General 3D structures solved using FEM www.dlubal.com CED

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Sheet: 1

Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

STRUCTURAL ANALYSIS

PROJECTKABETE SPIRAL STAIRCASE

CLIENT

CREATED BY

Z

X

Y

Isometric

RFEM 5.01.0022 - General 3D structures solved using FEM www.dlubal.com

CED

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Sheet: 1

MODEL

Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

CONTENTS Model - General Data 2 LC2: live, Isometric 9

1 Model CO2: 1.35*LC1 + 1.5*LC2, Isometric 91.1 Nodes 2 4 Results - Load Cases, Load1.2 Lines 3 Combinations1.3 Materials 5 4.0 Results - Summary 101.4 Surfaces 5 Deformations uZ, LC1: dead, Isometric 101.8 Line Supports 6 RF-CONCRETE Surfaces2 Load Cases and Combinations 1.1 General Data 112.1 Load Cases 6 1.2 Materials 112.1.1 Load Cases - Calculation Parameters 6 1.3 Surfaces 112.5 Load Combinations 6 RF-CONCRETE Surfaces - Required Reinforcement a-s,

1,-z (top), CA1, Isometric12

2.5.2 Load Combinations - Calculation Parameters 6 RF-CONCRETE Surfaces - Required Reinforcement a-s,2,-z (top), CA1, Isometric

13

2.6 Result Combinations 7 RF-CONCRETE Surfaces - Required Reinforcement a-s,1,+z (bottom), CA1, Isometric

13

3 Loads RF-CONCRETE Surfaces - Required Reinforcement a-s,2,+z (bottom), CA1, Isometric

14

3.4 Surface Loads 8 RF-CONCRETE Surfaces, CA1, Isometric 14 LC1: dead, Isometric 8 RF-CONCRETE Surfaces - Shear force ratio V-Ed /

V-Rd,max, CA1, Isometric15

3.4 Surface Loads 8

MODEL - GENERAL DATAGeneral Model name : spiral -kabete4

Project name : SPIRALFolder : C:\Users\Public\Documents\Dlubal\Projects\Examples\SPIRALType of model : 3DPositive direction of global axis Z : UpwardClassification of load cases and : According to Standard: EN 1990combinations National annex: BS - United Kingdom

Create automatically combinations : Load Combinations

1.1 NODESNode Reference Coordinate Node CoordinatesNo. Node Type Node System X [m] Y [m] Z [m] Comment

1 Standard - Cartesian 0.554 0.230 0.2192 Standard - Cartesian 0.600 0.000 0.0003 Standard - Cartesian 1.275 0.000 0.0004 Standard - Cartesian 1.178 0.488 0.2195 Standard - Cartesian 1.950 0.000 0.0006 Standard - Cartesian 1.802 0.746 0.2197 Standard - Cartesian 2.625 0.000 0.0008 Standard - Cartesian 2.425 1.005 0.2199 Standard - Cartesian 3.300 0.000 0.000

10 Standard - Cartesian 3.049 1.263 0.21911 Standard - Cartesian 0.424 0.424 0.43812 Standard - Cartesian 0.902 0.902 0.43813 Standard - Cartesian 1.379 1.379 0.43814 Standard - Cartesian 1.856 1.856 0.43815 Standard - Cartesian 2.333 2.333 0.43816 Standard - Cartesian 0.230 0.554 0.65617 Standard - Cartesian 0.488 1.178 0.65618 Standard - Cartesian 0.746 1.802 0.65619 Standard - Cartesian 1.005 2.425 0.65620 Standard - Cartesian 1.263 3.049 0.65621 Standard - Cartesian 0.000 0.600 0.87522 Standard - Cartesian 0.000 1.275 0.87523 Standard - Cartesian 0.000 1.950 0.87524 Standard - Cartesian 0.000 2.625 0.87525 Standard - Cartesian 0.000 3.300 0.87526 Standard - Cartesian -0.230 0.554 1.09427 Standard - Cartesian -0.488 1.178 1.09428 Standard - Cartesian -0.746 1.802 1.09429 Standard - Cartesian -1.005 2.425 1.09430 Standard - Cartesian -1.263 3.049 1.09431 Standard - Cartesian -0.424 0.424 1.31332 Standard - Cartesian -0.902 0.902 1.31333 Standard - Cartesian -1.379 1.379 1.31334 Standard - Cartesian -1.856 1.856 1.31335 Standard - Cartesian -2.333 2.333 1.31336 Standard - Cartesian -0.554 0.230 1.53137 Standard - Cartesian -1.178 0.488 1.53138 Standard - Cartesian -1.802 0.746 1.53139 Standard - Cartesian -2.425 1.005 1.53140 Standard - Cartesian -3.049 1.263 1.53141 Standard - Cartesian -0.600 0.000 1.75042 Standard - Cartesian -1.275 0.000 1.75043 Standard - Cartesian -1.950 0.000 1.75044 Standard - Cartesian -2.625 0.000 1.75045 Standard - Cartesian -3.300 0.000 1.75046 Standard - Cartesian -0.554 -0.230 1.969

Cartesian

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Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

1.1 NODESNode Reference Coordinate Node CoordinatesNo. Node Type Node System X [m] Y [m] Z [m] Comment47 Standard - Cartesian -1.178 -0.488 1.96948 Standard - Cartesian -1.802 -0.746 1.96949 Standard - Cartesian -2.425 -1.005 1.96950 Standard - Cartesian -3.049 -1.263 1.96951 Standard - Cartesian -0.424 -0.424 2.18852 Standard - Cartesian -0.902 -0.902 2.18853 Standard - Cartesian -1.379 -1.379 2.18854 Standard - Cartesian -1.856 -1.856 2.18855 Standard - Cartesian -2.333 -2.333 2.18856 Standard - Cartesian -0.230 -0.554 2.40657 Standard - Cartesian -0.488 -1.178 2.40658 Standard - Cartesian -0.746 -1.802 2.40659 Standard - Cartesian -1.005 -2.425 2.40660 Standard - Cartesian -1.263 -3.049 2.40661 Standard - Cartesian 0.000 -0.600 2.62562 Standard - Cartesian 0.000 -1.275 2.62563 Standard - Cartesian 0.000 -1.950 2.62564 Standard - Cartesian 0.000 -2.625 2.62565 Standard - Cartesian 0.000 -3.300 2.62566 Standard - Cartesian 0.230 -0.554 2.84467 Standard - Cartesian 0.488 -1.178 2.84468 Standard - Cartesian 0.746 -1.802 2.84469 Standard - Cartesian 1.005 -2.425 2.84470 Standard - Cartesian 1.263 -3.049 2.84471 Standard - Cartesian 0.424 -0.424 3.06372 Standard - Cartesian 0.902 -0.902 3.06373 Standard - Cartesian 1.379 -1.379 3.06374 Standard - Cartesian 1.856 -1.856 3.06375 Standard - Cartesian 2.333 -2.333 3.06376 Standard - Cartesian 0.554 -0.230 3.28177 Standard - Cartesian 1.178 -0.488 3.28178 Standard - Cartesian 1.802 -0.746 3.28179 Standard - Cartesian 2.425 -1.005 3.28180 Standard - Cartesian 3.049 -1.263 3.28181 Standard - Cartesian 0.600 0.000 3.50082 Standard - Cartesian 1.275 0.000 3.50083 Standard - Cartesian 1.950 0.000 3.50084 Standard - Cartesian 2.625 0.000 3.50085 Standard - Cartesian 3.300 0.000 3.50086 Standard - Cartesian 0.327 0.489 0.547

1.2 LINESLine Line LengthNo. Line Type Nodes No. L [m] Comment

1 Polyline 2,3 0.675 X2 Polyline 3,5 0.675 X3 Polyline 5,7 0.675 X4 Polyline 7,9 0.675 X5 Polyline 9,10 1.3066 Polyline 10,15 1.3067 Polyline 15,20 1.3068 Polyline 20,25 1.3069 Polyline 25,30 1.306

10 Polyline 30,35 1.30611 Polyline 35,40 1.30612 Polyline 40,45 1.30613 Polyline 45,50 1.30614 Polyline 50,55 1.30615 Polyline 55,60 1.30616 Polyline 60,65 1.30617 Polyline 65,70 1.30618 Polyline 70,75 1.30619 Polyline 75,80 1.30620 Polyline 80,85 1.30621 Polyline 85,84 0.675 X22 Polyline 84,83 0.675 X23 Polyline 83,82 0.675 X24 Polyline 82,81 0.675 X25 Polyline 81,76 0.32026 Polyline 76,71 0.32027 Polyline 71,66 0.32028 Polyline 66,61 0.32029 Polyline 61,56 0.32030 Polyline 56,51 0.32031 Polyline 51,46 0.32032 Polyline 46,41 0.32033 Polyline 41,36 0.32034 Polyline 36,31 0.32035 Polyline 31,26 0.32036 Polyline 26,21 0.32037 Polyline 21,16 0.32038 Polyline 16,86 0.160

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Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

1.2 LINESLine Line LengthNo. Line Type Nodes No. L [m] Comment39 Polyline 11,1 0.32040 Polyline 1,2 0.32041 Polyline 1,4 0.675 XY42 Polyline 4,6 0.675 XY43 Polyline 6,8 0.675 XY44 Polyline 8,10 0.675 XY45 Polyline 86,12 0.71646 Polyline 12,13 0.675 XY47 Polyline 13,14 0.675 XY48 Polyline 14,15 0.675 XY49 Polyline 16,17 0.675 XY50 Polyline 17,18 0.675 XY51 Polyline 18,19 0.675 XY52 Polyline 19,20 0.675 XY53 Polyline 21,22 0.675 Y54 Polyline 22,23 0.675 Y55 Polyline 23,24 0.675 Y56 Polyline 24,25 0.675 Y57 Polyline 26,27 0.675 XY58 Polyline 27,28 0.675 XY59 Polyline 28,29 0.675 XY60 Polyline 29,30 0.675 XY61 Polyline 31,32 0.675 XY62 Polyline 32,33 0.675 XY63 Polyline 33,34 0.675 XY64 Polyline 34,35 0.675 XY65 Polyline 36,37 0.675 XY66 Polyline 37,38 0.675 XY67 Polyline 38,39 0.675 XY68 Polyline 39,40 0.675 XY69 Polyline 41,42 0.675 X70 Polyline 42,43 0.675 X71 Polyline 43,44 0.675 X72 Polyline 44,45 0.675 X73 Polyline 46,47 0.675 XY74 Polyline 47,48 0.675 XY75 Polyline 48,49 0.675 XY76 Polyline 49,50 0.675 XY77 Polyline 51,52 0.675 XY78 Polyline 52,53 0.675 XY79 Polyline 53,54 0.675 XY80 Polyline 54,55 0.675 XY81 Polyline 56,57 0.675 XY82 Polyline 57,58 0.675 XY83 Polyline 58,59 0.675 XY84 Polyline 59,60 0.675 XY85 Polyline 61,62 0.675 Y86 Polyline 62,63 0.675 Y87 Polyline 63,64 0.675 Y88 Polyline 64,65 0.675 Y89 Polyline 66,67 0.675 XY90 Polyline 67,68 0.675 XY91 Polyline 68,69 0.675 XY92 Polyline 69,70 0.675 XY93 Polyline 71,72 0.675 XY94 Polyline 72,73 0.675 XY95 Polyline 73,74 0.675 XY96 Polyline 74,75 0.675 XY97 Polyline 76,77 0.675 XY98 Polyline 77,78 0.675 XY99 Polyline 78,79 0.675 XY100 Polyline 79,80 0.675 XY101 Polyline 7,8 1.047102 Polyline 8,14 1.047103 Polyline 14,19 1.047104 Polyline 19,24 1.047105 Polyline 24,29 1.047106 Polyline 29,34 1.047107 Polyline 34,39 1.047108 Polyline 39,44 1.047109 Polyline 44,49 1.047110 Polyline 49,54 1.047111 Polyline 54,59 1.047112 Polyline 59,64 1.047113 Polyline 64,69 1.047114 Polyline 86,11 0.160115 Polyline 74,79 1.047116 Polyline 79,84 1.047117 Polyline 69,74 1.047118 Polyline 5,6 0.792119 Polyline 6,13 0.792120 Polyline 11,4 0.787121 Polyline 1,1 0.000122 Polyline 23,28 0.792123 Polyline 28,33 0.792

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Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

1.2 LINESLine Line LengthNo. Line Type Nodes No. L [m] Comment124 Polyline 33,38 0.792125 Polyline 38,43 0.792126 Polyline 43,48 0.792127 Polyline 48,53 0.792128 Polyline 53,58 0.792129 Polyline 58,63 0.792130 Polyline 63,68 0.792131 Polyline 68,73 0.792132 Polyline 73,78 0.792133 Polyline 78,83 0.792134 Polyline 82,77 0.543135 Polyline 77,72 0.543136 Polyline 72,67 0.543137 Polyline 67,62 0.543138 Polyline 62,57 0.543139 Polyline 57,52 0.543140 Polyline 52,47 0.543141 Polyline 47,42 0.543142 Polyline 42,37 0.543143 Polyline 37,32 0.543144 Polyline 32,27 0.543145 Polyline 27,22 0.543146 Polyline 22,17 0.543147 Polyline 17,12 0.543148 Polyline 12,4 0.543149 Polyline 4,3 0.543150 Polyline 13,18 0.792151 Polyline 18,23 0.792

1.3 MATERIALSMatl. Modulus Modulus Poisson's Ratio Spec. Weight Therm. Coeff. Partial Factor MaterialNo. E [kN/cm2] G [kN/cm2] [-] [kN/m3] [1/°C] M [-] Model

1 Concrete C20/25 | BS EN 1992-1-1/NA:2005-123000.00 1250.00 0.200 24.00 1.0000E-05 1.000 Isotropic Linear Elastic

1.4 SURFACESSurface Surface Type Matl. Thickness Area Weight

No. Geometry Stiffness Boundary Lines No. No. Type d [mm] A [m2] W [kg]1 Quadrangle Standard 41,40,1,149 1 Constant 250.0 0.287 172.502 Quadrangle Standard 149,2,118,42 1 Constant 250.0 0.443 265.753 Quadrangle Standard 43,118,3,101 1 Constant 250.0 0.609 365.664 Quadrangle Standard 101,4,5,44 1 Constant 250.0 0.780 467.725 Quadrangle Standard 6,44,102,48 1 Constant 250.0 0.779 467.546 Quadrangle Standard 43,119,47,102 1 Constant 250.0 0.609 365.427 Quadrangle Standard 119,46,148,42 1 Constant 250.0 0.442 265.418 Quadrangle Standard 150,50,147,46 1 Constant 250.0 0.443 265.759 Quadrangle Standard 47,150,51,103 1 Constant 250.0 0.609 365.66

10 Quadrangle Standard 103,52,7,48 1 Constant 250.0 0.780 467.7211 Quadrangle Standard 54,146,50,151 1 Constant 250.0 0.443 265.7512 Quadrangle Standard 51,151,55,104 1 Constant 250.0 0.609 365.6613 Quadrangle Standard 52,104,56,8 1 Constant 250.0 0.780 467.7214 Quadrangle Standard 54,145,58,122 1 Constant 250.0 0.443 265.7515 Quadrangle Standard 55,122,59,105 1 Constant 250.0 0.609 365.6616 Quadrangle Standard 56,105,60,9 1 Constant 250.0 0.780 467.7217 Quadrangle Standard 106,60,10,64 1 Constant 250.0 0.779 467.5418 Quadrangle Standard 63,106,59,123 1 Constant 250.0 0.609 365.4219 Quadrangle Standard 62,123,58,144 1 Constant 250.0 0.442 265.4120 Quadrangle Standard 143,62,124,66 1 Constant 250.0 0.443 265.7521 Quadrangle Standard 124,67,107,63 1 Constant 250.0 0.609 365.6622 Quadrangle Standard 68,11,64,107 1 Constant 250.0 0.780 467.7223 Quadrangle Standard 12,72,108,68 1 Constant 250.0 0.779 467.5424 Quadrangle Standard 71,108,67,125 1 Constant 250.0 0.609 365.4225 Quadrangle Standard 70,125,66,142 1 Constant 250.0 0.442 265.4126 Quadrangle Standard 13,76,109,72 1 Constant 250.0 0.779 467.5427 Quadrangle Standard 110,76,14,80 1 Constant 250.0 0.779 467.5428 Quadrangle Standard 111,80,15,84 1 Constant 250.0 0.779 467.5429 Quadrangle Standard 112,84,16,88 1 Constant 250.0 0.779 467.5430 Quadrangle Standard 113,88,17,92 1 Constant 250.0 0.779 467.5431 Quadrangle Standard 117,92,18,96 1 Constant 250.0 0.779 467.5432 Quadrangle Standard 115,96,19,100 1 Constant 250.0 0.779 467.5433 Quadrangle Standard 100,20,21,116 1 Constant 250.0 0.779 467.5434 Quadrangle Standard 22,133,99,116 1 Constant 250.0 0.609 365.4235 Quadrangle Standard 132,99,115,95 1 Constant 250.0 0.609 365.4236 Quadrangle Standard 117,95,131,91 1 Constant 250.0 0.609 365.4237 Quadrangle Standard 130,87,113,91 1 Constant 250.0 0.609 365.4238 Quadrangle Standard 87,112,83,129 1 Constant 250.0 0.609 365.4239 Quadrangle Standard 83,111,79,128 1 Constant 250.0 0.609 365.4240 Quadrangle Standard 79,110,75,127 1 Constant 250.0 0.609 365.4241 Quadrangle Standard 126,75,109,71 1 Constant 250.0 0.609 365.42

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Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

1.4 SURFACESSurface Surface Type Matl. Thickness Area Weight

No. Geometry Stiffness Boundary Lines No. No. Type d [mm] A [m2] W [kg]42 Quadrangle Standard 37,49,146,53 1 Constant 250.0 0.287 172.5043 Quadrangle Standard 145,57,36,53 1 Constant 250.0 0.287 172.5044 Quadrangle Standard 144,61,35,57 1 Constant 250.0 0.287 171.9145 Quadrangle Standard 143,65,34,61 1 Constant 250.0 0.287 172.5046 Quadrangle Standard 142,69,33,65 1 Constant 250.0 0.287 171.9147 Quadrangle Standard 141,73,32,69 1 Constant 250.0 0.287 171.9148 Quadrangle Standard 126,74,141,70 1 Constant 250.0 0.442 265.4149 Quadrangle Standard 78,127,74,140 1 Constant 250.0 0.442 265.4150 Quadrangle Standard 140,77,31,73 1 Constant 250.0 0.287 171.9151 Quadrangle Standard 82,128,78,139 1 Constant 250.0 0.442 265.4152 Quadrangle Standard 81,139,77,30 1 Constant 250.0 0.287 171.9153 Quadrangle Standard 86,138,82,129 1 Constant 250.0 0.442 265.4154 Quadrangle Standard 85,138,81,29 1 Constant 250.0 0.287 171.9155 Quadrangle Standard 130,90,137,86 1 Constant 250.0 0.442 265.4156 Quadrangle Standard 28,89,137,85 1 Constant 250.0 0.287 171.9157 Quadrangle Standard 136,90,131,94 1 Constant 250.0 0.442 265.4158 Quadrangle Standard 27,89,136,93 1 Constant 250.0 0.287 171.9159 Quadrangle Standard 98,132,94,135 1 Constant 250.0 0.442 265.4160 Quadrangle Standard 97,135,93,26 1 Constant 250.0 0.287 171.9161 Quadrangle Standard 134,98,133,23 1 Constant 250.0 0.442 265.4162 Quadrangle Standard 134,24,25,97 1 Constant 250.0 0.287 171.9163 Quadrangle Standard 41,120,39,121 1 Constant 250.0 0.107 64.2264 Quadrangle Standard 114,120,148,45 1 Constant 250.0 0.235 140.8565 Quadrangle Standard 38,45,147,49 1 Constant 250.0 0.233 140.04

1.8 LINE SUPPORTSSupport Reference Rotation Wall Support Conditions

No. Lines No. System [°] in Z uX uY uZ X Y Z

1 Global3 1-4,21-24 Global

2.1 LOAD CASESLoad Load Case EN 1990 | BS Self-Weight - Factor in DirectionCase Description Action Category Active X Y ZLC1 dead Permanent 0.000 0.000 -1.000LC2 live Imposed - Category A: domestic,

residential areas

2.1.1 LOAD CASES - CALCULATION PARAMETERSLoad Load CaseCase Description Calculation parametersLC1 dead Method of analysis : Geometrically linear static analysis

Method for solving system of nonlinear algebraic equations

: Newton-Raphson

LC2 live Method of analysis : Geometrically linear static analysisMethod for solving system of nonlinear algebraic equations

: Newton-Raphson

2.5 LOAD COMBINATIONSLoad

Combin. Description No. Factor Load CaseCO1 1.35*LC1 1 1.35 LC1 deadCO2 1.35*LC1 + 1.5*LC2 1 1.35 LC1 dead

2 1.50 LC2 liveCO3 LC1 1 1.00 LC1 deadCO4 LC1 + LC2 1 1.00 LC1 dead

2 1.00 LC2 liveCO5 LC1 1 1.00 LC1 deadCO6 LC1 + 0.5*LC2 1 1.00 LC1 dead

2 0.50 LC2 liveCO7 LC1 1 1.00 LC1 deadCO8 LC1 + 0.3*LC2 1 1.00 LC1 dead

2 0.30 LC2 live

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LOADS

Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

2.5.2 LOAD COMBINATIONS - CALCULATION PARAMETERSLoad

Combin. Description Calculation parametersCO1 1.35*LC1 Method of analysis : Second order analysis (P-Delta)

Method for solving system of nonlinear algebraic equations

: Picard

Options : Consider favorable effects due to tension: Refer internal forces to deformed system for:

Normal forces NShear forces Vy and Vz

Moments My, Mz and MT

CO2 1.35*LC1 + 1.5*LC2 Method of analysis : Second order analysis (P-Delta)Method for solving system of nonlinear algebraic equations

: Picard

Options : Consider favorable effects due to tension: Refer internal forces to deformed system for:

Normal forces NShear forces Vy and Vz

Moments My, Mz and MT

CO3 LC1 Method of analysis : Second order analysis (P-Delta)Method for solving system of nonlinear algebraic equations

: Picard

Options : Consider favorable effects due to tension: Refer internal forces to deformed system for:

Normal forces NShear forces Vy and Vz

Moments My, Mz and MT

CO4 LC1 + LC2 Method of analysis : Second order analysis (P-Delta)Method for solving system of nonlinear algebraic equations

: Picard

Options : Consider favorable effects due to tension: Refer internal forces to deformed system for:

Normal forces NShear forces Vy and Vz

Moments My, Mz and MT

CO5 LC1 Method of analysis : Second order analysis (P-Delta)Method for solving system of nonlinear algebraic equations

: Picard

Options : Consider favorable effects due to tension: Refer internal forces to deformed system for:

Normal forces NShear forces Vy and Vz

Moments My, Mz and MT

CO6 LC1 + 0.5*LC2 Method of analysis : Second order analysis (P-Delta)Method for solving system of nonlinear algebraic equations

: Picard

Options : Consider favorable effects due to tension: Refer internal forces to deformed system for:

Normal forces NShear forces Vy and Vz

Moments My, Mz and MT

CO7 LC1 Method of analysis : Second order analysis (P-Delta)Method for solving system of nonlinear algebraic equations

: Picard

Options : Consider favorable effects due to tension: Refer internal forces to deformed system for:

Normal forces NShear forces Vy and Vz

Moments My, Mz and MT

CO8 LC1 + 0.3*LC2 Method of analysis : Second order analysis (P-Delta)Method for solving system of nonlinear algebraic equations

: Picard

Options : Consider favorable effects due to tension: Refer internal forces to deformed system for:

Normal forces NShear forces Vy and Vz

Moments My, Mz and MT

2.6 RESULT COMBINATIONSResult Result Combination Alternate

Combin. DS Description No. Factor Loading Criterion GroupRC1 ULS ULS (STR/GEO) - Permanent

/ transient - Eq. 6.101 1.00 CO1 Permanent 1

2 1.00 CO2 Permanent 1RC2 S Ch SLS - Characteristic 1 1.00 CO3 Permanent 1

2 1.00 CO4 Permanent 1RC3 S Fr SLS - Frequent 1 1.00 CO5 Permanent 1

2 1.00 CO6 Permanent 1RC4 S Qp SLS - Quasi-permanent 1 1.00 CO7 Permanent 1

2 1.00 CO8 Permanent 1

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LOADS

Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

3.4 SURFACE LOADS LC1

Load Load Load Load ParametersNo. On Surfaces No. Type Distribution Direction Symbol Value Unit

1 1-65 Force Uniform ZL p1 -2.50 kN/m2

LC1: DEAD, ISOMETRIC

2.50 2.50

2.50 2.50

2.50 2.50

2.50

X

Z

Y

2.50

2.50 2.50 2.50

2.50

2.50

2.50 2.50

2.50 2.50

2.50 2.50

2.50 2.50

2.50

2.50 2.50 2.50 2.50

2.50 2.50

2.50

2.50

2.50

2.50

2.50 2.50

2.50 2.50

2.50 2.50

2.50 2.50 2.50 2.50

2.50 2.50

2.50

2.50

2.50 2.50

2.50 2.50 2.50

2.50

2.50

2.50 2.50

2.50

2.50

2.50

2.50 2.50 2.50

2.50

2.50 2.50 2.50

IsometricLC1: dead

LC1: DEAD, ISOMETRIC

3.4 SURFACE LOADS LC2

Load Load Load Load ParametersNo. On Surfaces No. Type Distribution Direction Symbol Value Unit

1 1-65 Force Uniform ZL p1 -3.00 kN/m2

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LC2: LIVE, ISOMETRIC

3.00 3.00

3.00 3.00

3.00 3.00

3.00

X

Z

Y

3.00

3.00 3.00 3.00

3.00

3.00

3.00 3.00

3.00 3.00

3.00 3.00

3.00 3.00

3.00

3.00 3.00 3.00 3.00

3.00 3.00

3.00

3.00

3.00

3.00

3.00 3.00

3.00 3.00

3.00 3.00

3.00 3.00 3.00 3.00

3.00 3.00

3.00

3.00

3.00 3.00

3.00 3.00 3.00

3.00

3.00

3.00 3.00

3.00

3.00

3.00

3.00 3.00 3.00

3.00

3.00 3.00 3.00

IsometricLC2: live

LC2: LIVE, ISOMETRIC

CO2: 1.35*LC1 + 1.5*LC2, ISOMETRIC

3.38 3.38

3.38 3.38

4.50

3.38 3.38

3.38 3.38

X

Z

Y

4.50

4.50

3.38

4.50

3.38 3.38

3.38

3.38

3.38 3.38

3.38 3.38

3.38 3.38

4.50 4.50

4.50

3.38 3.38

3.38

3.38 3.38

4.50

4.50

3.38

4.50

3.38

3.38

4.50

3.38

3.38

4.50

4.50

4.50 4.50

4.50 4.50

3.38

4.50

3.38

3.38

4.50

3.38

4.50

3.38 3.38

3.38

4.50

4.50

4.50

3.38

4.50

3.38

4.50 4.50

4.50

3.38 3.38

4.50

4.50

3.38 3.38

3.38

4.50

3.38

4.50

3.38

3.38

3.38

4.50

4.50 4.50

4.50 4.50

4.50 4.50

3.38

3.38 3.38

4.50

3.38

3.38

4.50 4.50 4.50

4.50

3.38

4.50

4.50

4.50

4.50

3.38 3.38

3.38

3.38

3.38

4.50

4.50 4.50 4.50

4.50

3.38 3.38 3.38

4.50

4.50 4.50

4.50

4.50

4.50

3.38

3.38 3.38 3.38

4.50 4.50 4.50

4.50

4.50 4.50 4.50

IsometricCO2: 1.35*LC1 + 1.5*LC2

CO2: 1.35*LC1 + 1.5*LC2, ISOMETRIC

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Page: 10/15

Sheet: 1

RESULTS

Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

4.0 RESULTS - SUMMARYSummaryOther Settings Number of 1D finite elements : 0

Number of 2D finite elements : 216Number of 3D finite elements : 0Number of FE mesh nodes : 140Number of equations : 840Max. number of iterations : 100Number of divisions for member results : 10Division of cable/foundation/tapered members : 10Number of member divisions for searching maximum values : 10Subdivisions of FE mesh for graphical results : 3Percentage of iterations according to Picard method in combination with Newton-Raphson method

: 5 %

Options Activate shear stiffness of members (Ay, Az)Activate member divisions for large deformation or post-critical analysisActivate entered stiffness modificationsIgnore rotational degrees of freedomCheck of critical forces of members

Method for the system of equations DirectIteration

Plate bending theory MindlinKirchhoff

Solver version 32-bit64-bit

Precision and Tolerance Change default setting

DEFORMATIONS UZ

, LC1: DEAD, ISOMETRIC

-2.6

2.50 2.50

2.50 2.50

2.50 2.50

2.50

X

Z

Y

2.50

2.50 2.50 2.50

2.50

2.50

2.50 2.50

2.50 2.50

2.50 2.50

2.50 2.50

2.50

2.50 2.50 2.50 2.50

2.50 2.50

2.50

2.50

2.50

2.50

2.50 2.50

2.50 2.50

2.50 2.50

2.50 2.50 2.50 2.50

2.50 2.50

2.50

2.50

2.50 2.50

2.50 2.50 2.50

2.50

2.50

2.50 2.50

2.50

2.50

2.50

2.50 2.50 2.50

2.50

2.50 2.50 2.50

IsometricLC1: deadSupport Reactionsu-Z

Factor of deformations: 350.00Max u-Z: 0.0, Min u-Z: -2.6 [mm]

DEFORMATIONS UZ

, LC1: DEAD, ISOMETRIC

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Sheet: 1

RF-CONCRETE Surfaces

Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

1.1 GENERAL DATA

Design according to Standard: BS EN 1992-1-1/NA:2004

ULTIMATE LIMIT STATE

Load combinations for design: CO2 1.35*LC1 + 1.5*LC2

DETAILSAnalysis Method for Reinforcement Envelope MixedApply the averaged internal forces in the defined average region for the ULS calculation and for the analytic method of SLS calculation.Apply the internal forces without the rib components

1.2 MATERIALSMaterial Material Description

No. Concrete Strength Class Steel Description Comment1 Concrete C20/25 B 450 S (A)

1.3 SURFACESSurface Matl. Thickness Thickness

No. No. Type [cm] Notes Comment1 1 Constant 25.002 1 Constant 25.003 1 Constant 25.004 1 Constant 25.005 1 Constant 25.006 1 Constant 25.007 1 Constant 25.008 1 Constant 25.009 1 Constant 25.00

10 1 Constant 25.0011 1 Constant 25.0012 1 Constant 25.0013 1 Constant 25.0014 1 Constant 25.0015 1 Constant 25.0016 1 Constant 25.0017 1 Constant 25.0018 1 Constant 25.0019 1 Constant 25.0020 1 Constant 25.0021 1 Constant 25.0022 1 Constant 25.0023 1 Constant 25.0024 1 Constant 25.0025 1 Constant 25.0026 1 Constant 25.0027 1 Constant 25.0028 1 Constant 25.0029 1 Constant 25.0030 1 Constant 25.0031 1 Constant 25.0032 1 Constant 25.0033 1 Constant 25.0034 1 Constant 25.0035 1 Constant 25.0036 1 Constant 25.0037 1 Constant 25.0038 1 Constant 25.0039 1 Constant 25.0040 1 Constant 25.0041 1 Constant 25.0042 1 Constant 25.0043 1 Constant 25.0044 1 Constant 25.0045 1 Constant 25.0046 1 Constant 25.0047 1 Constant 25.0048 1 Constant 25.0049 1 Constant 25.0050 1 Constant 25.0051 1 Constant 25.0052 1 Constant 25.0053 1 Constant 25.0054 1 Constant 25.0055 1 Constant 25.0056 1 Constant 25.0057 1 Constant 25.0058 1 Constant 25.0059 1 Constant 25.0060 1 Constant 25.00

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Sheet: 1

RF-CONCRETE Surfaces

Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

1.3 SURFACESSurface Matl. Thickness Thickness

No. No. Type [cm] Notes Comment61 1 Constant 25.0062 1 Constant 25.0063 1 Constant 25.0064 1 Constant 25.0065 1 Constant 25.00

RF-CONCRETE SURFACES - REQUIRED REINFORCEMENT A-S,1,-Z (TOP),CA1, ISOMETRIC

RequiredReinforcementa-s,1,-z (top)[mm 2 /m]

669.790

608.900

548.010

487.120

426.230

365.340

304.450

243.560

182.670

121.780

60.890

0.000

Max : 669.790Min : 0.000

Z

X

Y

IsometricRF-CONCRETE Surfaces CA1Reinforced concrete designa-s,1,-z (top)

Max a-s,1,-z (top): 669.790, Min a-s,1,-z (top): 0.000 [mm2/m]

RF-CONCRETE SURFACES - REQUIRED REINFORCEMENT A-S,1,-Z (TOP),CA1, ISOMETRIC

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Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

RF-CONCRETE SURFACES - REQUIRED REINFORCEMENT A-S,2,-Z (TOP),CA1, ISOMETRIC

RequiredReinforcementa-s,2,-z (top)[mm 2 /m]

669.790

608.900

548.010

487.120

426.230

365.340

304.450

243.560

182.670

121.780

60.890

0.000

Max : 669.790Min : 0.000

Z

X

Y

IsometricRF-CONCRETE Surfaces CA1Reinforced concrete designa-s,2,-z (top)

Max a-s,2,-z (top): 892.732, Min a-s,2,-z (top): 0.000 [mm2/m]

RF-CONCRETE SURFACES - REQUIRED REINFORCEMENT A-S,2,-Z (TOP),CA1, ISOMETRIC

RF-CONCRETE SURFACES - REQUIRED REINFORCEMENT A-S,1,+Z(BOTTOM), CA1, ISOMETRIC

RequiredReinforcementa-s,1,+z (bottom)[mm 2 /m]

669.790

608.900

548.010

487.120

426.230

365.340

304.450

243.560

182.670

121.780

60.890

0.000

Max : 669.790Min : 0.000

Z

X

Y

IsometricRF-CONCRETE Surfaces CA1Reinforced concrete designa-s,1,+z (bottom)

Max a-s,1,+z (bottom): 763.973, Min a-s,1,+z (bottom): 0.000 [mm2/m]

RF-CONCRETE SURFACES - REQUIRED REINFORCEMENT A-S,1,+Z(BOTTOM), CA1, ISOMETRIC

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Sheet: 1

Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

RF-CONCRETE SURFACES - REQUIRED REINFORCEMENT A-S,2,+Z(BOTTOM), CA1, ISOMETRIC

RequiredReinforcementa-s,2,+z (bottom)[mm 2 /m]

669.790

608.900

548.010

487.120

426.230

365.340

304.450

243.560

182.670

121.780

60.890

0.000

Max : 669.790Min : 0.000

Z

X

Y

IsometricRF-CONCRETE Surfaces CA1Reinforced concrete designa-s,2,+z (bottom)

Max a-s,2,+z (bottom): 2664.982, Min a-s,2,+z (bottom): 0.000 [mm2/m]

RF-CONCRETE SURFACES - REQUIRED REINFORCEMENT A-S,2,+Z(BOTTOM), CA1, ISOMETRIC

RF-CONCRETE SURFACES, CA1, ISOMETRIC

Z

X

Y

IsometricRF-CONCRETE Surfaces CA1Reinforced concrete design

RF-CONCRETE SURFACES, CA1, ISOMETRIC

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Date: 8/7/2015 Project: SPIRAL Model: spiral -kabete4

RF-CONCRETE SURFACES - SHEAR FORCE RATIO V-ED / V-RD,MAX, CA1,ISOMETRIC

Shear force ratioV-Ed / #0000210106#V-Rd,max[-]

0.001

0.001

0.001

0.000

0.000

0.000

0.000

0.000

0.000

0.000

0.000

0.000

Max : 0.001Min : 0.000

Z

X

Y

IsometricRF-CONCRETE Surfaces CA1Reinforced concrete designV-Ed / V-Rd,max

Max V-Ed / V-Rd,max: 0.735, Min V-Ed / V-Rd,max: 0.001 [-]

RF-CONCRETE SURFACES - SHEAR FORCE RATIO V-ED / V-RD,MAX, CA1,ISOMETRIC

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