franky anak ajie - universiti malaysia sarawak comparison between eurocode 3 (1992) and... · a...
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A COMPARISON BETWEEN EUROCODE 3 (1992) AND BRITISH STANDARD 5950 (2000) FOR FLEXURAL MEMBER DESIGN
FRANKY ANAK AJIE
..
This project is submitted in partial fulfil1ment of . the requirements for the degree of Bachelor of Engineering with Honours
(Civil Engineering)
,.• Faculty of Engineering UNIVERSITY MALAYSIA SARA WAK
2006
I
To my beloved parents, Ajie Anak Lang and Ungo Anak Bilong
•
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ACKNOWLEDGEMENT
.,'"
The following people have made significant contributions to the writing of this
project and their assistance is acknowledged with grateful thank.
The author is grateful to thesis supervisor, Puan Azida Rashidi for her guidance
and advices throughout the project.
Not forget also to thank the author's parents, Ajie Anak Lang and Ungo Anak
Bilong who give financial support until the completion of the project.
Finally, thanks once again to everyone who has helped in contributing ideas and
advices throughout the entire project. Thank you very much .
11l I
ABSTRACT
The European Standards and British Standards are the standards used in design of
structural steeL This project is about the comparisons between the two standards
with respect to a flexural member design. The European Standards used for this
project is the Eurocode 3: Part 1.1 (1992) or simply written as EC 3: Part 1.1
(1992). While, the British Standards used in this project is the BS 5950: Part 1
(2000). There are few methods of comparison used in this project. These methods
include the notation, load factors, load combinations and design considerations, an
example of flexural member design, the safety factors, economical factors,
advantages and disadvantages of the two standards. Throughout the project, it is
found that the notations used are slightly different from each standard. The limit
states design is the design basis for both standards. The factors considered in
flexural member design include shear capacity, bending moment capacity, web
buckling capacity, web bearing capacity or web crushing capacity and deflection.
For the EC 3: Part 1.1 (1992), an extra check on web crippling and maximum
deflection, ornax which is not required in the BS 5950: Part 1 (2000). From the
results, it can be concluded that the EC 3: Part 1.1 (1992) is more conservative
while the BS 5950: Part 1 (2000) is more economical. However, in the real
practice, both of the standards offer almost the same results in term of
conservativeness and economical factor.
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ABSTRAK
European Standards dan British Standards merupakan piawaian yang
digunakan untuk merekabentuk struktur binaan. Projek ini membincangkan
perbezaan di antara kedua-dua piawaan dengan merekabentuk angota lenturan.
European Standards yang digunakan dalam projek ini ialah Eurocode 3: Part 1.1
(1992) atau ringkasnya ditulis sebagai EC 3: Part 1.1 (1992). Manakala British
Standards yang digunakan dalam project ini ialah BS 5950: Part 1 (2000).
Beberapa kaedah telah digunakan dalam projek ini. Ini termasuklah perbandingan
simbol-simbol yang digunakan, perbandingan faktor beban, perbandingan
gabungan factor beban dan pertimbangan merekabentuk, perbandingan
menggunakan contoh merekabentuk angota lenturan, perbandingan dari segi
faktor keselamatan, faktor economi dan perbandingan kebaikan and keburukan
antara kedua-dua piawaian tersebut. Melalui projek ini, diketahui bahawa
kebanyakan simbol-simbol yang digunakan dalam kedua-dua piawaian agak
berlainan antara satu sarna lain. Rekabentuk keadaan had muktamad dan had
khidmad merupakan dasar rekabentuk untuk kedua-dua piawaian. Faktor-faktor
yang dipertimbangkan dalam angota lenturan termasuk keupayaan ricih,
keupayaan lenturan, web buckling capacity, web bearing capacity atau web
crushing capacity dan pesongan. Untuk EC 3: Part /.1 (1992) semakan tambahan
ke atas web crippling dan pesongan maximum, omax perlu dilakukan, semakan ini
tidak diperlukan di dalam BS 5950: Part 1 (2000). Daripada keputusan yang
diperolehi, dapat disimpulkan bahawa EC 3: Part 1.1 (1992) lebih konservatif
manakala BS 5950: Part 1 (2000) lebih jimat dari segi ekonomi. Walau
bagaimanapun, dalam situasi sebenar, kedua-dua piawai akan memberikan
keputusan yang hampir sama dari segi factor konservatif and ekonomi.
.",
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TABLE OF CONTENT
Page
TITLE i
DEDICATION ii
ACKNOWLEDGEMENT iii
ABSTRACT iv
ABSTRAK v
TABLE OF CONTENT vi-ix
LIST OF FIGURES x
LIST OF TABLES xi-xii
LIST OF SYMBOLS xiii-xviii
LIST OF ABBREVIATION xix
Chapter 1 INTRODUCTION
1.1 Background 1-3
'- 1.2 Significance of Study 4
1.3 Aim and Objective 5
.... 1.4 Scope of Study, 6
1.5 Conclusion 6
VI
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Chapter 2 LITERATURE REVIEW
2.1 Introduction 7
2.2 The Standards 7
2.2.1 European Standard - EC 3: Part 1.1 (1992) 8
2.2.2 British Standard - BS 5950: Part 1 (2000) 8
2.3 Structure Design Basis 8
2.3.1 Load Factors and Combinations for the EC 3: Part 1.1 (1992) 10-11
2.3.2 Load Factors and Combinations for the BS 5950: Part 1 (2000) 12 -13
2.4 Partial Safety Factors for materials 13
2.4.1 Partial Safety Factors for materials for the EC 3: Part 1.1 (1992) 13-14
2.4.2 Partial Safety Factors for materials for the BS 5950: Part 1 (2000) 14
2.5 Flexural Member Design Consideration 14
2.5.1 Flexural Member Design Consideration for the EC 3: Part 1.1 (1992) 15-24
2.5.1 Flexural Member Design Consideration for the BS 5950: Part 1 (2000) 25-34
2.6 Conclusion 35
Chapter 3 METHODOLOGY
3.1 Introduction 36
3.2 Methods of comparison 36 ... 3.2.1 Notation 36
3.2.2 Load factors, load combinations and
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Chapter 4
Chapter 5
.... !
design consideration
3.2.3 A case study of flexural member design
3.2.4 The safety factors, economical factors, advantages and disadvantages of the two standards
3.4 Conclusion
DESIGN EXAMPLES
4.1 Introduction
4.2 Design examples
4.3 Design using EC 3: Part 1.1 (1992) for simply supported restrained beam
4.4 Design using BS 5950: Part 1 (2000) for simply supported restrained beam
4.5 Design using EC 3: Part 1.1 (1992) for simply supported unrestrained beam
4.6 Design using BS 5950: Part 1 (2000) for simply supported unrestrained beam
4.7 Conclusion
RESULTS AND DISCUSSION
5.1 Introduction
5.2 Terminology
5.2.1 Decimal Point
5.2.2 Actions
5.2.3 Resistance
5.2.4 Subscripts
5.2.5 Design Philosophy
37
37-39
40
40
41
41-42
43-52
53-62
63-72
73-81
82
83
83
84
84
85
85
86
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Chapter 6
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5.2.6 Partial Load Factors 86
5.2.7 Load Factors and combination 87-90
5.2.8 Partial Safety Factors 91-92
5.3 Symbols 92-93
5.4 Conventions 93-94
5.5 Material and Elastic Modulus 94-96
5.6 Limiting shear stress and limiting shear capacity 96-98
5.7 Summary of results obtained from Chapter 4 98-99
5.8 Conclusion 100
CONCLUSIONS AND RECOMMENDATIONS
6.1 Introduction 101
6.2 Problems Faced 101
6.3 Conclusion 102-104
6.4 Recommendations 105
REFERENCES 107-108
APPENDIX A 109-116
APPENDIXB 116-122
APPENDIXC 123
APPENDIXD 124-125
IX I
,..... ... e
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Figures
2.1
3.1
5.1
5.2
5.3
5.4
5.5
5.6
LIST OF FIGURES
Pages
Vertical Deflection 24
Simply Supported Beam 38
Actual load consist ofdead load and imposed load. 88
Actual load consist ofdead load and wind load 89
Actual load consist ofdead load, imposed load and 90 wind load.
Comparison ofmembers axes between EC 3: Part 1.1 (1992) 94 and BS 5950: Part 1 (2000)
Limiting shear stress 97
Limiting shear capacity 97
x
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Tables
2.1
2.2
2.3
2.4
2.5
2.6
2.7
2.8
2.9
5.1
5.2 'I':,
5.3
• 5.4
5.5
LIST OF TABLES
Pages
Limit States - BS 5950: Part: 1 (2000) 9
Design value of action for use in the combination of actions 11
Partial safety factors for actions on building structures for 11 persistent and transient design situations.
Partial factors for loads, 'Yf 12
Maximum width - to - thickness ratios for compression elements 15
Recommended limiting values for vertical deflection. 23
Classification of cross section 25
Limiting width to thickness ratios 26
Limits for calculated deflection 34
Comparison in term of decimal point 84
Comparison in term of action is called in the two standards 84
Comparison in term ofresistance is called in the two codes 85
Partial Load Factors 87
Partial Safety Factors for materials, EC 3: Part 1.1 (1992) 91
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5.6 Partial Safety Factors for materials, BS 5950: Part 1 (2000) 91
5.7 Symbols used in the EC 3: Part 1.1 (1992) and 93 BS 5950: Part 1 (2000)
5.8 Comparison of shear capacity 96
5.9 Summary of Design - Total design loads 98
5.10 Summary of Design Shear Capacity 98
5.11 Summary of Design - Bending Moment 99
5.12 Summary of Design - Bearing Capacity 99
5.13 Summary ofDesign Deflection 99
XlI
p AX i¢
LIST OF SYMBOLS
Symbols used in this project - EC 3: Part 1.1 (1992)
Latin upper case letters
A -Accidental action
A - Area
C - Capacity; Fixed value; Factor
E - Modulus of elasticity
F - Action
F - Force
G - Pennanent action
G - Shear modulus
I - Second moment of area
K - Stiffness factor (l/L)
L - Length; Span; System length
M - Moment in general
M - Bending moment
N - Axial force
Q - Variable action
R - Resistance; Reaction
S -Internal forces and moments (with subscripts d or k)
S - Stiffness (shear, rotational ... stiffness with subscripts v, j ...)
T - Torsional moment; Temperature
V - Shear force; Total vertical load or reaction ;Ilf:,
W - Section modulus
Latin lower case letters
a-Distance; Geometrical data
a -Area ratio
Xlll I
--- --..,.....-
b -Width; Breadth
c -Distance; Outstand
d -Diameter; Depth; Length of diagonal
e -Eccentricity
e -Edge distance; End distance
f -Strength (of a material)
h -Height
-Radius of gyration
k -Coefficient; Factor
-(or I or L) Length; Span; Buckling lengtha
a J (lower case L) can be replaced by L or by = (handwritten) for certain lengths or to avoid confusion with I (numeral) or I (upper case i)
n -Ratio ofnormal forces or normal stresses
p -Pitch; Spacing
q -Uniformly distributed force
r -Radius; Root radius
s -Staggered pitch; Distance
t -Thickness
xx -Axis along member
yy -Axis of cross-section
zz -Axis of cross-section
Greek lower case letters
a -(alpha) Angle; Ratio; Factor
y -(gamma) Partial safety factor; Ratio
o -(delta) Deflection; Deformation
-(epsilon) Strain; Coefficient [235/fy)O,5 (fy in N/mm2)
-(eta) Coefficient (in Annex E)
-(lambda) Slenderness ratio; Ratio
-emu) Slip factor; Factor
v -(nu) Poisson's ratio
p -(rho) Reduction factor; Unit mass
XIV
a -(sigma) Nonnal stress
't -(tau) Shear stress
¢ -(phi) Rotation; Slope; Ratio
X -(chi) Reduction factor (for buckling)
\jI -(psi) Stress ratio; Reduction factor or Factors defining representative
values ofvariable actions.
Subscripts
A
a
b
C
c
cr
d
E
eff
e
el
f
g
G
h
h
i, j, k
~" k
I
LT
Mr M
m
-Accidental; Area
-Average (yield strength)
-Bearing; Buckling
-Capacity; Consequences
-Cross section
-Critical
-Design; Diagonal
-Euler
-Effective
-Effective (with further subscript)
-Elastic
-Flange; Fastener
-Gross
-Pennanent action
-Height; Higher
-Horizontal
-Inner
-Indices (replace by numeral)
-Characteristic
-Lower
-Lateral-torsional
-Material
-(Allowing for) bending moment
-Bending
xv
max
mm
N
pI
Q
R
s
V
x
y
Y
z
-Maximum
-Minimum
-(Allowing for) axial force
-Plastic
-Variable action
-Resistance
-Stiff; Stiffener
-(Allowing for) shear force
-Axis along member; Extension
-Yield
-Axis of cross-section
-Axis of cross-section
XVl
l
,... ,
Symbols used in this project - BS 5950: Part 1 (2000)
A -Area
Ae -Effective net area
AetT -Effective cross-sectional area
Av -Shear area of a member
a -Spacing of transverse stiffeners
B -Width
b -Outstand
D -Depth of section or Diameter of section
d -Depth ofweb
E -Modulus of elasticity of steel
e -Edge or end distance
Fv -Shear force in a member
fc -Compressive stress due to axial force
fv -Shear stress
H -Warping constant of section
h -Height
Ixx -Second moment ofarea about the major axis
Iyy -Second moment of area about the minor axis
J -Torsion constant of section
L -Length or Span
LE -Effective length
M -Moment
Mb -Buckling resistance moment (lateral-torsional buckling)
Me -Moment capacity
m -Equivalent uniform moment factor
Pc -Compression resistance
P v -Shear capacity of a member
Pb -Bending strength (lateral-torsional buckling)
Pc -Compressive strength
py -Design strength ofsteel
qw -Shear buckling strength of a web
XVll
" p
rx -Radius of gyration about the major axis
ry -Radius of gyration about the minor axis
Seff -Effective plastic modulus
Sx -Plastic modulus about the major axis
Sy -Plastic modulus about the minor axis
T -Thickness of a flange
t -Thickness or Thickness of a web
u -Buckling parameter of a cross-section
Vb -Shear buckling resistance of a web
Vcr -Critical shear buckling resistance of a web
v -Slenderness factor for a beam
x-Torsional index of a cross-section
Zeff -Effective section modulus
Zx -Section modulus about the major axis (minimum value unless otherwise
stated)
Zy -Section modulus about the minor axis (minimum value unless otherwise
stated)
'Yf -Overall load factor
e -Constant (275/py)O.5
J... -Slenderness, i.e. the effective length divided by the radius of gyration
Acr -Elastic critical load factor
ALO -Limiting equivalent slenderness (lateral-torsional buckling)
ALI -Equivalent slenderness (lateral-torsional buckling)
AO -Limiting slenderness (axial compression)
XVlll
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LIST OF ABBREVIATION
AL - Actual load
AM - Allowable moment
AS Allowable shear
ASD Allowable strength design
AW - Allowable web
BS - British standard
CIDB Construction Industry Development Board
DL Design Load
DM - Design Moment
DS - Design Shear
DW -Design Web
LFC - Load Factor and Combination
LRFD - Load and resistance factor design
LSD - Limit state design
MC - Moment Capacity
NARB- National Association ofRome Builders
RF - Reduction Factor
SC Shear Capacity
WC - Web Capacity
XIX
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CHAPTERl
INTRODUCTION
1.1 Background
Steel is one of the principle materials used in designing buildings and civil
engineering works such as bridges and towers. There are five types of structural
steelwork that are widely used in the construction of buildings and civil
engineering works. These are carbon steels, alloy steels, high-strength low-alloy
steels, stainless steels and tools steels. Each types of steel exhibits different
characteristics such as strength, ductility, hardness, and corrosion resistance.
Steels are usually more economical, recyclable, long life, easy to transport and
handle on site.
There are several steel standards used all over the world, such as the
American Iron and Steel Institute Standards, Australian and New Zealand
Standards, Japanese Standards, British Standards and European Standards or
Eurocodes. In this project work, the Eurocodes and British Standards will be used.
The Eurocodes are the European Standards applied in designing of structural
design. The European Standards that will be used for this project work is the
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Eurocode 3 (1992) or simply written as EC 3 (1992). It applies to the design of
buildings and civil engineering works in steeL This standard came into effect on
15 November 1992 and was published by the European Committee for
Standardization (CEN) and the National Application Document (NAD) to be used
with the European Pre-Standard (ENV) for the design of buildings to be
constructed in the United Kingdom. Like the BS 5950 (2000), EC 3 (1992) comes
in a number of parts and covers a range of application. It consists of the following
Parts:
Part 1.1: General rules and rules for buildings.
Part 1.2: Fire resistance.
Part 1.3: Cold formed thin gauge members and sheeting.
Part 2 : Bridges and plated structures.
Part 3 : Towers, masts and chimneys.
Part 4 : Tanks, silos and pipelines.
Part 5 : Piling.
Part 6 : Cranes structures.
Part 7 : Marine and maritime structures.
Part 8 : Agricultural structures.
Part 1.1 of EC 3 (1992) gives a general basis for the design of buildings and
civil engineering works in steel. The remaining Parts of the code (Part 1.2 to Part
8) are generally related to specifications or to specialist types of construction and
will not be mentioned further in this project work.
2
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The British Standards for steel that will be used in this project work is the BS
5950 (2000). It is the principal source of guidance for the design of structural
steelwork in the United Kingdom and is widely used in Malaysia. This standard
has been prepared under the direction of the Civil Engineering and Building
Structures Standards Policy Committee and was published under the authority of
the Standard Committee B/525/31 in May 2001. It replaces the BS 5950 (1990)
which is withdrawn. BS 5950 (2000) edition introduces technical changes based
on the review of the BS 5950 (1990). BS 5950 (2000) comprise of the following
Parts:
Part 1: Code of practice for design: Rolled and welded sections.
Part 2: Specification for materials, fabrication and erection: Rolled and
welded sections.
Part 3: Design in composite construction Section 3.1: Code of practice for
design of simple and continuous composite beams.
Part 4: Code of practice for design of composite slabs with profiled steel
sheeting.
Part 5: Code of practice for design of cold formed thin gauge sections.
Part 6: Code of practice for design of light gauge profiled steel sheeting.
Part 7: Specification for materials, fabrication and erection: Cold formed
sections and sheeting.
Part 8: Code of practice for fire resistant design.
Part 9: Code of practice for stressed skin design.
3
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BS 5950 (2000): Part 1 gives recommendations for the design of simple and
continuous steel structures, using rolled and welded sections. The remaining Parts
of the code (Part 2 to Part 9) are generally related to specifications or to specialist
types of construction and will not be mentioned further in this project work.
In this project work, the comparison is made between the EC 3: Part 1.1
(1992) and BS 5950: Part 1 (2000). The flexural member design is taken as an
example of calculation to show the differences. The scopes of the comparison will
be discussed further in Section 1.4 of this chapter.
1.2 Significance of study
According to a journal by Sooi and Teoh (2004), the EC 3 (1992) will
replace BS 5950 (2000) in the year 2008 in the United Kingdom. It is envisioned
that the process of transition from the usage of BS 5950 (2000) to EC 3 (1992) in
Malaysia will run parallel with that in the United Kingdom.
The adoption of EC 3 (1992) could help the local construction industry and
practicing engineers in gaining access to the latest technology in steel engineering
practices. They could also be able to get updates since the EC 3 (1992) documents
would have regular maintenance. Another advantage in adopting EC 3 (1992) is
its ready alignment with International Standards Organization or ISO, in term of
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format and coverage. EC 3 (1992) has unique features, such as National Annexes,
formally referred to as National Application Documents (NAD).
As Malaysia always uses British Standards as the main resource of reference
and since the British has decided to align with the European Union with the
adoption of EC 3 (1992), it would be prudent for Malaysia to follow suit.
1.3 Aim and objectives
The aim of this project work is to alleviate the learning curve through the
comparison of the design approaches and the parametric studies of the two
standards. This will ensure a smooth and easier transition of the BS 5950 (2000)
to the EC 3: (1992).
Thus, the objectives are:
(a) To compare the notations, limit state design and design considerations
between the two standards.
(b) To show the simplified design method ofEC 3: Part 1.1 (1992).,
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(c) To show the simplified design method ofBS 5950: Part 1 (2000).
'<\'.0
l I (d) To compare the design methods for flexural member design between
the two standards.
(e) To determine the advantages and disadvantages of each standards.
I (f) To compare the safety and economy aspects between the two standards
by using an example of flexural member design as a case study.
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1.4 Scopes of study
This study is limited to:
(a) The Ee 3 Part 1.1 (1992) and BS 5950 Part 1 (2000).
(b) Only the flexural member design is considered as a case study.
(c) The ultimate limit state and serviceability limit state only.
(d) Only hot-rolled steel member is considered.
1.5 Conclusion
Hence, it is very important for local construction industry and practicing
engineer to understand the significance of the transition of BS 5950 (2000) to Ee
3 (1992). This will help our local construction industry and practicing engineers to
get equipped and ready to the adoption of the Ee 3 (1992) in the year 2008. In the
next chapters, we will discuss more detail about the Ee 3: Part 1.1 (1992) and the
BS 5950: Part 1 (2000).
6
CHAPTER 2
LITERATURE REVIEW
2.1 Introduction
This chapter describes about the EC 3: Part 1.1 (1992) and BS 5950: Partl
(2000) in general. It highlights the differences between the two standards based on
design basis and member design considerations with respect to flexural member
design.
2.2 The standards
As mentioned earlier in Section 1.1 of Chapter 1, there are many standards
for the design of structural steel all over the world. Thus, in this project work, the
comparison between the EC 3: Part 1.1 (1992) and the BS 5950: Partl (2000) for
t flexural member design will be studied.
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2.2.1 European Standard - EC3: Part 1.1 (1992)
The European Standard used in this project work is EC 3: Part 1.1 (1992). It
gives a general basis for the design of buildings and civil engineering works in
steel. This standard is published by the European Committee for Standardization
(CEN) and the National Application Document (NAD) and come into effect on 15
November 2000. It is to be used with the European Pre-Standard (ENV) for the
design of buildings to be constructed in the United Kingdom.
2.2.2 British Standard - BS 5950: Part 1 (2000)
The British Standard used in this project work is BS 5950: Part 1 (2000).
This standard has been prepared under the direction of the Civil Engineering and
Building Structures Standards Policy Committee and was published under the
authority of the Standard Committee B/525/31 in May 2001. It replaces the BS
5950: Part 1 (1990) which is now withdrawn. BS 5950: Part 1 (2000) gives
recommendations for the design of simple and continues steel structures using
rolled and welded sections.
2.3 Standards Design Basis
The design basis in structural steel design is based on the limit states concept.
This design basis is used in both of the standards, EC 3: Part 1.1 (1992) and BS
5950: Part 1 (2000).
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According to Clause 2.1.3 BS 5950: Part 1 (2000), structures should be
designed by considering the limit states beyond which they would become unfit
for their intended use. There are two types of limit states to be taken into account
in the limit states design, ultimate limit states and serviceability limit states.
According to the BS 5950: Part 1 (2000), ultimate limit states concern the safety
of the whole or part of the structure while serviceability limit states correspond to
limits beyond which specified service criteria are no longer met.
Therefore, the design is done based on the strength and stability at ultimate
loading. After the design was done, the deflection will be checked under the
serviceability loading. Table 2.1 outlines the typical limit states appropriate to
steel structures.
Table 2.1: Limit States
Ultimate limit states (ULS) Serviceability limit states (SLS) Strength (including yielding, rapture, Deflection.
buckling and forming a mechanism).
Stability against overturning and sway . Vibration.
stability.
Fracture due to fatigue. Wind induced oscillation.
IBrittle fracture. I Durability.
[Source: BS5950: Part 1 (2000)]
In a flexural member design, factors such as material strength loading and
structural performance will be taken into account. For analysis purposes, partial
load factors should be applied to the working or nominal loads of dead load,
9
imposed load and wind load in order to minimize the failure of the structures.
These factors are applied based on the load factors and combinations. The load
factors and combinations of the two standards will be discussed further in Section
2.3.1 and Section 2.3.2 for the EC 3: Part 1.1 (1992) and the BS 5950: Part 1
(2000) respectively.
2.3.1 Load Factors and Combinations for the EC 3: Part 1.1 (1992)
The Eurocode provides indicative values for various safety factors and are
shown in the text as "boxed values" 1.35
According to Chanakya Arya (1994), the values in the box D signify
that these values may be used by individual member state for time being. This
system of identifying certain parameters was introduced in order to account for
national differences in material properties, design and construction practices and
climatic condition.
According to Clause 2.3.2.2 of EC 3: Part 1.1 (1992), load factors and
combinations are taken as shown in Table 2.2.
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r Table 2.2: Design values of actions for use in the combination of actions
[Source: EC 3: Part 1.1 (1992)]
To obtain the persistent and transient design situations, Clause 2.3.3 ofEC 3:
Part 1.1 (1992) shall follow. Table 2.3 below shows the partial safety factors for
actions on building structures for persistent and transient design situations.
For unfavourable effect, the permanent actions is multiplied by 1,35 and
variable actions is multiplied by 1,5.
Table 2.3: Partial safety factors for actions on building structures for persistent and transient design situations.
Permanent Variable actions Qd Accidental IDesign I situation actions Gd Leading Accompanying actions Ad Ii
I variable action variable action iPersistent and 'Po YQQkYGGk YQQk
Transient I Accidental 'P2QkYGAGk J 'PIQk YAAk
!
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Permanent actions (YG)
Variable actions (YG) Leading variable action
Accompanying variable action
Favourable effect YF inf 1,0 ** ** Unfavourable effect YF sup 1,35 1,5 1,5
: * See also 2.3.3.1 (3) ofEC 3: Part 1.1 (1992) I ** See Eurocode 1; in normal cases for building structures YQ,inf= °
[Source: EC 3: Part 1.1 (1992)]
Where,
Gk = is the characteristic values of the permanent actions
Qk is the characteristic values of the variable actions
11
= is the design value (specified value) of the accidental action
= is the partial safety factor for the permanent action Gk , ~
is the partial safety for accidental design situations, "fGA'~
= is the partial safety factor for the variable action Qk, ~
"fGA
"fQ
l'0,1' 1,1' 2 = Representative values of variable actions defined in Clause 2.2.2.3
ofEC 3: Part 1.1 (1992).
2.3.2 Load Factors and Combinations for the BS 5950: Part 1 (2000)
According to Clause 2.2 of BS 5950: Part 1 (2000), load factors and
combinations are taken as shown in Table 2.4.
Table 2.4: Partial factors for loads, "ff
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I
Loading Factor, 'Yf I Dead load 1.4
I Dead load when restraining sliding, overturning or uplift 1.0
Dead load acting together with wind load and imposed load
combined
1.2
Imposed load 1.6
Imposed load acting together with wind load 1.2
Wind load 1.4
Wind load acting together with imposed load 1.2
Forces due to temperature change 1.2
[Source: BS5950: Part 1 (2000)]
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r I I t
To obtain the design load at ultimate limit state, the load is multiplied by the
load factor obtained from Table 2.4. The dead load is multiplied by 1.4 and
imposed load multiplied by 1.6. When wind load is considered the dead load,
imposed load and wind load are multiplied by 1.2.
According to Clause 2.5 of BS 5950: Part 1 (2000), when considering the
combination of dead load, imposed load and wind load, only 80% of the imposed
load and wind will be considered.
2.4 Partial Safety Factors for materials
The values used in partial safety factors for materials in the both codes, EC 3:
Part 1.1 (1992) and BS 5950: Part 1 (2000) are different from one another. These
differences are explained in section 2.4.1 and section 2.4.2 respectively.
2.4.1 Partial Safety Factors for materials, EC 3: Part 1.1 (1992)
When considering combinations of loads consisting of more than one
variable load, EC 3: Part 1.1 (1992) adopts a method utilizing a combination
factor, 'P. According to Clause 5.1.1 of the EC 3: Part 1.1 (1992), the partial safety
factors for materials are taken as different values as shown below,
I 13
l
Resistance of class 1, 2 or 3 cross section, 'YMO = ~
Resistance of class 4 cross section 'YMI ~
Resistance of member to buckling 'YMI ~
Resistance of net section at bolt holes 'YM2 = ~
2.4.2 Partial Safety Factor for materials, BS 5950: Part 1 (2000)
According to Clause 2.1.3 of the BS 5950: Part 1 (2000), the material factor
is taken as 1.0 applied to the yield strength or 1.2 applied to the tensile strength
for structural steel.
2.5 Flexural Member Design Consideration
Generally, the EC 3: Part 1.1 (1992) and the BS 5950: Part 1 (2000) consider
almost the same design parameters in structural member design. The design
parameters considered in the EC 3: Part 1.1 (1992) are section classification, shear
resistant, moment resistant, web buckling, web crushing web crippling and
deflection. While, the design parameters considered in the BS 5950: Part 1 (2000)
include section classification, shear capacity, moment capacity, web buckling,
web bearing and deflection. Section 2.5.1 and Section 2.5.2 will show how these
factors are determined by each standard.
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2.5.1 Flexural Member Design Considerations for the EC 3: Part 1.1 (1992)
The flexural member design considerations are illustrated as follow:
(1) Classification of cross-sections
According to Clause 5.3.2, there are four classifications of cross section used
in the EC 3: Part 1.1 (1992). There are class 1, class 2, class 3 and class 4. The
classification of a cross section depends upon the proportions of its compression
element. The classes are given as in Table 2.5.
Table 2.5: Maximum width - to - thickness ratios for compression elements
Class of elementI Type of element IClass 1 Class 2 Class 3
IC/tr:S lOs Cltr:S 118 Cltf:S 15s II Outstand flange
I: for rolled section I Wed with neutral d/tw:S 728 d/tw:S 83s d/tw:S 1248 . axis at mid depth, I
I rolled sectionjIWed subject to I d/tw:S 33s d/tw:S 388 d/tw:S 42s . compressIOn, i rolled section I
I275 N/mm.4Yield strength, fy I 235 N/mm.4 355 N/mmL
1Strain, s 0.92 0.81
[Source: EC3:Part1.1 (1992)]
The factor 8 is given by 8 = (235/fy)o.s. According to Clause 5.3.5 of EC 3:
Part 1.1 (1992), for class 3, sections effective cross sectional properties can be
calculated using effective widths ofthe compression element.
15
(2) Shear resistance
According to clause 5.6.1 of EC 3: Part 1.1 (1992), calculation for resistance
to shear buckling should be made when the depth-to-thickness ratio ditw is greater
than 69E for an unstiffened web or 30s(kt)o.s for a stiffened web.
Where; d = Depth of the web
tw Web thickness
E Strain, [235/fy]o.s. (fy in N/mm2)
kt = Buckling factor for shear
According to clauses 5.4.6 ofEC 3: Part 1.1 (1992), the design value of shear
force, Vsd should not greater then VpLRd.
Where; (2.1)
Av = Shear area for rolled I and H sections
Av =A - btr + (tw+2r)tr (2.2)
For simplicity, Av can be taken as I,04htw
A = Cross section area
b = Overall breadth
h = Depth of section
tf = Flange thickness
tw = Web thickness
r = Root radius
t
I I 16
(3) Moment capacity,
The design value of the bending moment, Msd, is obtained from the clause
5.4.5 ofEC 3: Part 1.1 (1992) should not exceed the moment of resistance of the
section, Me.Rd·
Me.Rd. may be taken as follow:
a) The design plastic resistance moment of the gross section
M p1•Rd = Wplfy / yMO (2.3)
Where; Mpl.Rd design plastic moment resistance of the gross
cross-section
Wplfy = the plastic section modulus, for class 1 and class 2
section only.
yMO = partial safety factor for resistance applies to failure by
yielding.
b) The design elastic resistance moment of the gross section
Mel•Rd = Welfy / yMO (2.4)
Where; Mcl.Rd = design elastic moment resistance of the gross cross
section
Wclfy = the elastic section modulus for class 3 sections.
17
yMO = partial safety factor for resistance applies to failure by
yielding.
c) The design local buckling resistance moment of the gross section
M o.Rd =WetTfy I yMl (2.5)
Where; MO.Rd design moment resistance of effective gross cross-
section
Wefffy = the effective section modulus, for class 4 cross
section only.
yMl = partial safety factor for resistance applies to all types
of buckling resistance of a member.
(4) Crippling resistance
For an I or H section, the design crippling resistance is;
- 0 5 2 Ef )1I2( 112Ra.Rd - • tw (yw (trltw) + 3(tw/tr)(sJd)1 yMl (2.6)
in which ss/d should not be more than 0.2. Where the member is also subject to
bending moments the following relationship should be satisfied;
Where; Ra.Rd = design crippling resistance
(2.7)
18
Fsd = design shear of resistance of the cross section
Mc,Rd = design moment of resistance of the cross section
Msd design value of bending moment
tw = thickness of web
E Modulus of Elasticity
fyw is the yield strength of the web
tr= is the flange thickness
ss = is the length of stiff bearing
d Depth of the web
yMI partial safety factor for resistance applies to all types
of buckling resistance of a member.
(5) Crushing resistance.
According to Clause 5.7.3 ofEC 3: Part 1.1 (1992), for an I or H section, the
design crushing resistance is;
(2.8)
Where; (2.9)
in which br should not be more than 25tr, ss is the length of stiff bearing and O"[Ed
is the longitudinal stress in the flange. Alternatively, Sy may be obtained from;
Sy =[ 2.5(h-d) (1-( O'f.Ed/fyc)2) 112 ) I [(1+0.8 ss) I (h-d) ) (2.10)
19
Where; Ry.Rd = design crushing resistance
Ss = is the length of stiff bearing
Sy is the effective length of stiffbearing
tw thickness of web
tf= is the flange thickness
bf = width of flange
fyw = is the yield strength of the web
VMl = partial safety factor for resistance applies to all types
of buckling resistance of a member.
O"f.Ed = is the longitudinal stress in the flange
(6) Lateral torsional buckling
In Clause 5.5.2 of EC 3: Part 1.1 (1992), the design buckling resistance
moment of a laterally unrestrained beam shall be taken as;
(2.11)
Where; XLT is the reduction factor for lateral torsional buckling
~w = 1 for Class 1 or Class 2 cross-sections
~w = WeLy! WpLy for Class 3 cross-sections
~w = Weff.y! Wpl.y for Class 4 cross-sections
WpLy plastic section modulus about the y-y axis
fy = is the yield strength
20
1Ml = partial safety factor for resistance applies to all types
of buckling resistance of a member.
Msd design value of bending moment
The value of reduction factor, XLT the appropriate non-dimensional
slenderness A LT may be determined from Table 5.5.2 of EC 3: Part 1.1 (1992)
which is attached at the Table A6 of Appendix A. with A = Au and X = XLT, using
curve a (a = 0,21) for rolled sections and curve c (a = 0,49) for welded sections.
Alternatively, the value of reduction factor, XLTmay be obtained from the equation
below.
1 (2.12)XLT = r 2 - 2 fl2 ~ 1
¢LT + L¢u - ALT
- - 2 in which, ¢u=0,5 [1 +ULT (Au -0,2)+ ALl' ] (2.13)
Where; XLT= is the reduction factor for lateral torsional buckling
¢LT rotation
AlX slenderness ratio
aLT= values of imperfect factor 0,21 for rolled sections and
0,49 for welded sections
The value slenderness ratio, ALT may be determined from,
(2.14)
21
Where; ~ = JT [E/fy]O,5 = 93,38 (2.15)
8 = [235/fy] (2.16)
fy 0::: is the yield strength
Pw = 1 for Class 1 or Class 2 cross-sections
Pw WeI./ Wpl.y for Class 3 cross-sections
Pw Weff.yl Wpl.y for Class 4 cross-sections
The geometrical slenderness ratio can be obtained from the equation below.
L[!VP1{]114 IJw
ALT = 114 (2.17)
C 112[1 + L2
GI/ ] I JT2 E1w
Where; L = length of the beam between points which lave lateral
restrained.
Wpl.yo::: plastic section modulus about the y-y axis
Iz = second moment of area about minor axis
Iy second moment of area about major axis
It 0::: torsional constant
Iw 0::: warping constant
E = Modulus of Elasticity
E G shear modulus, ( )
21+v
22