SKITSEPROJEKT - LandCAD

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C1.2A
C1.2C
C2.1A
C2.1D
C2.2A
C2.3A
C2.3D
C2.4
NED
NED1
ÅBNING
Job Number
Job Title
Client
Calcs by Checked by Date
Sheet
5324
Kulturbro-Aalborg - Bilag 2
Jens Toft-Nielsen
32
Morten Struve Nielsen Ejvind Rasmussen 19-03-2007
Comb. Load factor for each load case: Ultimate Limit State
DL LL VL
C1.1A 1.0 1.0 0.0
C1.1B 1.0 0.0 1.0
C1.2A 1.0 1.0 1.0
C1.2C 1.0 1.0 1.0
C2.1A 1.0 1.3 0.5
C2.1D 1.0 0.5 1.5
C2.2A 0.8 1.3 0.5
C2.3A 0.3 1.0 0.5
C2.3D 0.3 0.5 1.0
C2.4 1.0 1.1 1.3
NED 1.0 1.0 0.0
NED1 0.0 1.0 0.0
ÅBNING 1.0 0.0 0.0
Comb. Load factor for each load case: Serviceability Limit State
DL LL VL
C1.1A 1.0 0.4 0.0
C1.1B 1.0 0.0 0.4
C1.2A 1.0 0.8 0.5
C1.2C 1.0 0.4 0.6
C2.1A 1.0 1.0 1.0
C2.1D 1.0 1.0 1.0
C2.2A 1.0 1.0 1.0
C2.3A 1.0 1.0 1.0
C2.3D 1.0 1.0 1.0
C2.4 1.0 1.0 1.0
NED 1.0 1.0 0.0
NED1 0.0 1.0 0.0
ÅBNING 1.0 0.0 0.0
========================== OUTPUT: LINEAR ANALYSIS ============================
====================== NODAL POINT DISPLACEMENTS at SLS =======================
Node Lcase X-disp. Y-disp. Z-disp. X-rot. Y-rot. Z-rot.
mm mm mm rad. rad. rad.
1 DL -0.48 -0.00 -0.02 0.0000 0.0001 -0.0005
LL -2.90 -0.01 -0.19 0.0002 0.0002 -0.0031
VL 0.71 0.00 -0.01 0.0000 0.0003 0.0008
C1.1A -1.64 -0.00 -0.09 0.0001 0.0001 -0.0017
C1.1B -0.19 -0.00 -0.02 0.0000 0.0002 -0.0002
C1.2A -2.44 -0.01 -0.17 0.0002 0.0004 -0.0026
C1.2C -1.21 -0.00 -0.10 0.0001 0.0003 -0.0013
C2.1A -2.67 -0.01 -0.21 0.0002 0.0005 -0.0028
C2.1D -2.67 -0.01 -0.21 0.0002 0.0005 -0.0028
C2.2A -2.67 -0.01 -0.21 0.0002 0.0005 -0.0028
C2.3A -2.67 -0.01 -0.21 0.0002 0.0005 -0.0028
C2.3D -2.67 -0.01 -0.21 0.0002 0.0005 -0.0028
C2.4 -2.67 -0.01 -0.21 0.0002 0.0005 -0.0028
NED -3.38 -0.01 -0.20 0.0002 0.0003 -0.0036
NED1 -2.90 -0.01 -0.19 0.0002 0.0002 -0.0031
ÅBNING -0.48 -0.00 -0.02 0.0000 0.0001 -0.0005
2 DL 0.00 0.00 0.00 0.0000 -0.0000 -0.0003
LL 0.00 0.00 0.00 0.0002 -0.0000 -0.0018
VL 0.00 0.00 0.00 0.0000 -0.0001 0.0003
C1.1A 0.00 0.00 0.00 0.0001 -0.0000 -0.0010
C1.1B 0.00 0.00 0.00 0.0000 -0.0000 -0.0001
C1.2A 0.00 0.00 0.00 0.0002 -0.0000 -0.0015
C1.2C 0.00 0.00 0.00 0.0001 -0.0000 -0.0008
C2.1A 0.00 0.00 0.00 0.0002 -0.0001 -0.0017