Project: Model: Detail 02-L Profile

Cartesian 1.1 NODES

Node Reference Coordinate Node Coordinates
No. Node Type Node System X [m] Y [m] Z [m] Comment
1 Standard - Cartesian 0.000 0.045 -0.010
2 Standard - Cartesian -0.200 -0.125 0.090
3 Standard - Cartesian 0.000 0.045 0.090
4 Standard - Cartesian -0.200 0.045 0.090
5 Standard - Cartesian 0.000 -0.125 0.090
6 Standard - Cartesian 0.000 -0.125 -0.010
7 Standard - Cartesian 0.000 -0.040 0.005
8 Standard - Cartesian 0.000 -0.040 0.080
9 Standard - Cartesian 0.420 -0.040 0.005
10 Standard - Cartesian 0.420 -0.040 0.080
11 Standard - Cartesian 0.391 -0.040 0.040
16 Standard - Cartesian -0.162 0.015 0.090 Supported
18 Standard - Cartesian 0.341 -0.040 0.040
19 Standard - Cartesian 0.291 -0.040 0.040
20 Standard - Cartesian -0.162 -0.095 0.090 Supported

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 Node Numbering Isometric
Support Numbering

30
2
16

0.0
3
Project:

70
0.1
MODEL

d = 16.0 mm
2
20 8

30
2 Z
Y1

0.0
d = 16.0 mm
0 .03 8
5
7 X
d = 12.0 mm
19 10
18
11
0.075

6
9

0.100

RFEM 5.25.02 - General 3D structures solved using FEM

0 .05 0
0 .05 0
0 .02 9
Model: Detail 02-L Profile

0 .42 0

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Project: Model: Detail 02-L Profile

1.2 LINES
Line Line Length
No. Line Type Nodes No. L [m] Comment
1 Polyline 4,3 0.200 X
2 Polyline 3,1 0.100 Z
3 Polyline 2,5 0.200 X
4 Polyline 4,2 0.170 Y
5 Polyline 3,5 0.170 Y
6 Polyline 5,6 0.100 Z
7 Polyline 8,7 0.075 Z
8 Polyline 1,6 0.170 Y
9 Polyline 10,9 0.075 Z
10 Polyline 8,10 0.420 X
11 Polyline 7,9 0.420 X

1.3 MATERIALS
Matl. Modulus Modulus Poisson's Ratio Spec. Weight Coeff. of Th. Exp. Partial Factor Material
No. E [kN/cm 2] G [kN/cm 2]  [-]  [kN/m 3]  [1/°C] M [-] Model
1 Steel S 235 | EN 10025-2:2004-11
21000.00 8076.92 0.300 78.50 1.20E-05 1.00 Isotropic Linear
Elastic

1.4 SURFACES
Surface Surface Type Matl. Thickness Area Weight
No. Geometry Stiffness Boundary Lines No. No. Type d [mm] A [m2] W [kg]
2 Quadrangle Standard 1,5,3,4 1 Constant 16.0 0.034 4.27
3 Quadrangle Standard 2,8,6,5 1 Constant 16.0 0.017 2.14
4 Quadrangle Standard 7,11,9,10 1 Constant 12.0 0.032 2.97

1.4.2 SURFACES - INTEGRATED OBJECTS

Surface Integrated Objects No.
No. Nodes Lines Openings Comment
2 16,20
3 7
4 11,18,19

1.7 NODAL SUPPORTS

Support Column Support Conditions
No. Nodes No. Axis System in Z uX uY uZ X Y Z
2 16,20 Global X,Y,Z

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 Project: Model: Detail 02-L Profile

MODEL
Node Numbering Isometric

16 3

20 8
Z
2 Y1

5
7 X 10
19
18
11

9
6

MODEL
Line Numbering Isometric

4
2
Z
5
Y

3 7 10
X

8
6 11 9

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 Project: Model: Detail 02-L Profile

MODEL
Surface Numbering Isometric

S2
Z
Y

S3
X
S4

2.1 LOAD CASES

Load Load Case EN 1990 | SS Self-Weight - Factor in Direction
Case Description Action Category Active X Y Z
LC1 Design Load Permanent 0.000 0.000 -1.000
LC2 Permanent/Imposed

2.1.1 LOAD CASES

Load Load Case
Case Description Calculation Parameters
LC1 Design Load Method of analysis : Geometrically linear analysis
Method for solving system of : Newton-Raphson
nonlinear algebraic equations
Activate stiffness factors of: : Cross-sections (factor for J, Iy, I z, A, Ay, Az)
: Members (factor for GJ, EIy, EIz, EA, GA y, GAz)
LC2 Method of analysis : Geometrically linear analysis
Method for solving system of : Newton-Raphson
nonlinear algebraic equations
Activate stiffness factors of: : Cross-sections (factor for J, Iy, I z, A, Ay, Az)
: Members (factor for GJ, EIy, EIz, EA, GA y, GAz)

3.1 NODAL LOADS - BY COMPONENTS

LC1 - COORDINATE SYSTEM LC1: Design Load
Design Load On Nodes Coordinate Force [kN] Moment [kNm]
No. No. System PX / P U PY / PV PZ / P W MX / MU MY / MV MZ / MW
1 11,18,19 0 | Global XYZ 4.260 0.360 0.000 0.000 0.000 0.000

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 Project: Model: Detail 02-L Profile

LC1: DESIGN LOAD

LC1 : Design Load Isometric
Loads [kN]

d = 16.0 mm

Y
Z

d = 16.0 mm

X
4.260
4.260
4.260
d = 12.0 mm

0.360
0.360
0.360

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 Project: Model: Detail 02-L Profile

4.0 RESULTS - SUMMARY

Description Value Unit Comment
Load Case LC1 - Design Load
Sum of loads in X 12.78 kN
Sum of support reactions in X 12.78 kN Deviation 0.00%
Sum of loads in Y 1.08 kN
Sum of support reactions in Y 1.08 kN Deviation 0.00%
Sum of loads in Z -0.09 kN
Sum of support reactions in Z -0.09 kN Deviation -0.00%
Resultant of reactions about X 0.025 kNm At center of gravity of model (X:0.021, Y:-0.040, Z:0.064 m)
Resultant of reactions about Y -0.301 kNm At center of gravity of model
Resultant of reactions about Z 0.346 kNm At center of gravity of model
Max. displacement in X 0.9 mm FE Mesh Node No. 6 (X: 0.000, Y: -0.125, Z: -0.010 m)
Max. displacement in Y 8.5 mm FE Mesh Node No. 9 (X: 0.420, Y: -0.040, Z: 0.005 m)
Max. displacement in Z 4.5 mm FE Mesh Node No. 10 (X: 0.420, Y: -0.040, Z: 0.080 m)
Max. vector displacement 9.6 mm FE Mesh Node No. 9 (X: 0.420, Y: -0.040, Z: 0.005 m)
Max. rotation about X 1.6 mrad FE Mesh Node No. 34 (X: 0.105, Y: -0.040, Z: 0.080 m)
Max. rotation about Y -9.7 mrad FE Mesh Node No. 6 (X: 0.000, Y: -0.125, Z: -0.010 m)
Max. rotation about Z 28.0 mrad FE Mesh Node No. 9 (X: 0.420, Y: -0.040, Z: 0.005 m)
Maximum surface strain 0.000 ‰ FE Mesh Node No. 0 (X: 0.000, Y: 0.000, Z: 0.000 m)
Method of analysis Linear Geometrically linear analysis
Reduction of stiffness Cross-sections, Members, Surfaces
Number of load increments 1
Number of iterations 1
Maximum value of element of stiffness matrix on 3.641E+10
diagonal
Minimum value of element of stiffness matrix on 2.008E+05
diagonal
Stiffness matrix determinant 6.000E+1671
Infinity Norm 7.835E+10

Summary

Other Settings:
Number of 1D finite elements 0
Number of 2D finite elements 32
Number of 3D finite elements 0
Number of FE mesh nodes 40
Number of equations 240
Max. number of iterations 100
Number of divisions for member results 10
Division of cable/foundation/tapered members 10
Number of member divisions for searching 10
maximum values
Subdivisions of FE mesh for graphical results 3
Percentage of iterations according to Picard 5 %
method in combination with Newton-Raphson
method

Options:
Activate shear stiffness of members (Ay, Az)
Activate member divisions for large deformation or
post-critical analysis
Activate entered stiffness modifications
Ignore rotational degrees of freedom
Check of critical forces of members
Nonsymmetric direct solver if demanded by
nonlinear model
Method for the system of equations Direct
Plate bending theory Mindlin
Solver version 64-bit

Precision and Tolerance:

Change default setting

4.1 NODES - SUPPORT FORCES

Node Support Forces [kN] Support Moments [kNm]
No. LC/CO PX' PY' PZ' MX' MY' MZ'
16 LC1 1.15 -0.19 0.44 0.00 -0.33 -0.01 Design Load
20 LC1 11.63 1.27 -0.54 0.00 -0.29 -0.02 Design Load
 Supp. LC1 12.78 1.08 -0.09
 Loads LC1 12.78 1.08 -0.09

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 Project: Model: Detail 02-L Profile

SUPPORT REACTIONS
LC1 : Design Load Isometric
Support Reactions[kN]

0.44

1.27
1.15

Z
0.19 11.63 Y

0.54

Max P-X': 11.63, Min P-X': 1.15 kN

Max P-Y': 1.27, Min P-Y': -0.19 kN
Max P-Z': 0.44, Min P-Z': -0.54 kN

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 Project: Model: Detail 02-L Profile
RF-STEEL Surfaces
with selection
General stress analysis 1.1 GENERAL DATA
of steel surfaces Surfaces to design All
Load cases to design: LC1 Design Load

1.2 MATERIALS
Material Material Safety Factor Yield Strength Limit Stresses [kN/cm 2]
No. Description M [-] fyk [kN/cm 2] Manually Limit x Limit  Limit eqv limit eqv,m
1 Steel S 235 1.00 23.50 23.50 13.57 23.50 23.50

1.3 SURFACES
Surface Material Thickness Max Stress Area Weight
No. No. Type d [mm] Ratio A [m2] G [t] Comment
2 1 Constant 16.0 0.81 0.03 0.00
3 1 Constant 16.0 0.66 0.02 0.00
4 1 Constant 12.0 0.81 0.03 0.00

RF-STEEL Surfaces 2.2 STRESSES BY MATERIAL

with selection Material Surface FE Mesh Point Coordinates [m] Stress [kN/cm 2] Stress
General stress analysis No. No. Point No. X Y Z Loading Symbol Existing Limit Ratio [-]
of steel surfacesRESULTS 1 Steel S 235
4 7 0.000 -0.040 0.005 LC1 x,+ 19.00 23.50 0.81
3 3 0.000 0.045 0.090 LC1 y,+ 9.27 23.50 0.39
3 3 0.000 0.045 0.090 LC1 xy,+ -4.70 23.50 0.20
2 16 -0.162 0.015 0.090 LC1 x,- -18.90 23.50 0.80
3 3 0.000 0.045 0.090 LC1 y,- -9.54 23.50 0.41
2 16 -0.162 0.015 0.090 LC1 max 2.74 13.57 0.20
4 7 0.000 -0.040 0.005 LC1 1,+ 19.10 23.50 0.81
2 16 -0.162 0.015 0.090 LC1 2,+ -8.73 23.50 0.37
2 16 -0.162 0.015 0.090 LC1 1,- 7.98 23.50 0.34
2 16 -0.162 0.015 0.090 LC1 2,- -19.03 23.50 0.81
4 7 0.000 -0.040 0.005 LC1 1,m 2.26 23.50 0.10
4 8 0.000 -0.040 0.080 LC1 2,m -1.27 23.50 0.05
2 16 -0.162 0.015 0.090 LC1 eqv,max 17.23 23.50 0.73
4 7 0.000 -0.040 0.005 LC1 eqv,m 2.96 23.50 0.13

Ratio x,+
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-x,+ [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.81
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-x,+: 0.81, Min Ratio Sigma-x,+: 0.00 -

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 Project: Model: Detail 02-L Profile

Ratio y,+
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-y,+ [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.39
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-y,+: 0.39, Min Ratio Sigma-y,+: 0.00 -

Ratio xy,+
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-xy,+ [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.20
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-xy,+: 0.20, Min Ratio Sigma-xy,+: 0.00 -

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 Project: Model: Detail 02-L Profile

Ratio y,-
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-y,- [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.41
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-y,-: 0.41, Min Ratio Sigma-y,-: 0.00 -

Ratio xy,-
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-xy,- [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.22
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-xy,-: 0.22, Min Ratio Sigma-xy,-: 0.00 -

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 Project: Model: Detail 02-L Profile

Ratio eqv,max
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-eqv [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.73
0.01
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-eqv: 0.73, Min Ratio Sigma-eqv: 0.01 -

Ratio eqv,m
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-eqv,m [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.13
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-eqv,m: 0.13, Min Ratio Sigma-eqv,m: 0.00 -

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 Project: Model: Detail 02-L Profile

Ratio eqv,+
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-eqv,+ [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.72
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-eqv,+: 0.72, Min Ratio Sigma-eqv,+: 0.00 -

Ratio eqv,-
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Sigma-eqv,- [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.73
0.01
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Sigma-eqv,-: 0.73, Min Ratio Sigma-eqv,-: 0.01 -

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 Project: Model: Detail 02-L Profile

Ratio xz
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Tau-xz [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.20
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Tau-xz: 0.20, Min Ratio Tau-xz: 0.00 -

Ratio yz
RF-STEEL Surfaces CA1 Isometric
LC1
Stress Ratio
Tau-yz [-]

1.00

0.90

0.80

0.70

0.60

0.50

0.40

0.30 d = 16.0 mm
0.20

0.10

0.00
Z
Max :
Min :
0.14
0.00
Y
d = 16.0 mm

X
d = 12.0 mm

Max Ratio Tau-yz: 0.14, Min Ratio Tau-yz: 0.00 -

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