Eurocode 9: Design of aluminium structures - Part 1-1: General structural rules

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Date: 2020-06

prEN 1999-1-1:2021

CEN/TC 250 Secretariat: BSI

Eurocode 9: Design of aluminium structures - Part 1-1: General structural

rules

Eurocode 9: Calcul des structures en aluminium - Partie 1-1: Règles générales

Eurocode 9: Bemessung und Konstruktion von Aluminiumtragwerken - Teil 1-1: Allgemeine Bemessungsregeln ICS:

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European foreword

This document (prEN 1999-1-1:2021) has been prepared by Technical Committee CEN/TC250 "Structural Eurocodes", the secretariat of which is held by BSI. CEN/TC 250 is responsible for all Structural Eurocodes and has been assigned responsibility for structural and geotechnical design matters by CEN.

This document is currently submitted to the CEN Enquiry. This document will supersede EN 1999-1-1:2007.

The first generation of EN Eurocodes was published between 2002 and 2007. This document forms part of the second generation of the Eurocodes, which have been prepared under Mandate M/515 issued to CEN by the European Commission and the European Free Trade Association.

The Eurocodes have been drafted to be used in conjunction with relevant execution, material, product and test standards, and to identify requirements for execution, materials, products and testing that are relied upon by the Eurocodes.

The Eurocodes recognize the responsibility of each member State and have safeguarded their right to determine values related to regulatory safety matters at national level through the use of National Annexes.

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Introduction

0.1 Introduction to the Eurocodes

The Structural Eurocodes comprise the following standards generally consisting of a number of Parts: • EN 1990 Eurocode: Basis of structural and geotechnical design

• EN 1991 Eurocode 1: Actions on structures

• EN 1992 Eurocode 2: Design of concrete structures • EN 1993 Eurocode 3: Design of steel structures

• EN 1994 Eurocode 4: Design of composite steel and concrete structures • EN 1995 Eurocode 5: Design of timber structures

• EN 1996 Eurocode 6: Design of masonry structures • EN 1997 Eurocode 7: Geotechnical design

• EN 1998 Eurocode 8: Design of structures for earthquake resistance • EN 1999 Eurocode 9: Design of aluminium structures

• <New parts>

The Eurocodes are intended for use by designers, clients, manufacturers, constructors, relevant authorities (in exercising their duties in accordance with national or international regulations), educators, software developers, and committees drafting standards for related product, testing and execution standards.

NOTE Some aspects of design are most appropriately specified by relevant authorities or, where not specified, can be agreed on a project-specific basis between relevant parties such as designers and clients. The Eurocodes identify such aspects making explicit reference to relevant authorities and relevant parties.

0.2 Introduction to EN 1999 Eurocode 9

EN 1999 applies to the design of buildings and civil engineering and structural works made of aluminium. It complies with the principles and requirements for the safety and serviceability of structures, the basis of their design and verification that are given in EN 1990 – Basis of structural design.

EN 1999 is only concerned with requirements for resistance, serviceability, durability and fire resis-tance of aluminium structures. Other requirements, e.g. concerning thermal or sound insulation, are not considered.

EN 1999 does not cover the special requirements of seismic design. Provisions related to such requirements are given in EN 1998, which complements, and is consistent with EN 1999.

For the design of new structures, prEN 1999 is intended to be used, for direct application, together with EN 1990, EN 1991, EN 1992, EN 1993, EN 1994, EN 1995, EN 1997, EN 1998 and EN 1999.

EN 1999 is subdivided in five parts:

— EN 1999-1-1 Design of Aluminium Structures: General structural rules. — EN 1999-1-2 Design of Aluminium Structures: Structural fire design.

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— EN 1999-1-4 Design of Aluminium Structures: Cold-formed structural sheeting. — EN 1999-1-5 Design of Aluminium Structures: Shell structures.

0.3 Introduction to EN 1999-1-1

This document gives basic design rules for structures made of wrought aluminium alloys and limited guidance for cast alloys.

This document is the first of the five parts of EN 1999. It gives generic design rules that are intended to be used with the other parts EN 1999-1-2 to EN 1999-1-5.

EN 1999-1-1 can be used for design cases not covered by the Eurocodes (other structures, other actions, other materials) and serving as a reference document for other CEN TC´s concerning structural matters. 0.4 Verbal forms used in the Eurocodes

The verb “shall" expresses a requirement strictly to be followed and from which no deviation is permitted in order to comply with the Eurocodes.

The verb “should” expresses a highly recommended choice or course of action. Subject to national regulation and/or any relevant contractual provisions, alternative approaches could be used/adopted where technically justified.

The verb “may" expresses a course of action permissible within the limits of the Eurocodes.

The verb “can" expresses possibility and capability; it is used for statements of fact and clarification of concepts.

0.5 National annex for prEN 1999-1-1

National choice is allowed in this standard where explicitly stated within notes. National choice includes the selection of values for Nationally Determined Parameters (NDPs).

The national standard implementing EN 1999-1-1 can have a National Annex containing all national choices to be used for the design of buildings and civil engineering works to be constructed in the relevant country.

When no national choice is given, the default choice given in this standard is to be used.

When no national choice is made and no default is given in this standard, the choice can be specified by a relevant authority or, where not specified, agreed for a specific project by appropriate parties.

National choice is allowed in EN 1999-1-1 through the following clauses: — 4.1.2(3) NOTE — 4.4.3(2) NOTE — 4.5(1) NOTE — 5.2.1(1) NOTE — 5.2.2(2) NOTE 2 — 5.2.3.1(2) NOTE — 5.3.2.1(4) NOTE — 5.3.2.2(1) NOTE — 8.1.6.2(3) NOTE

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— 9.1(3) NOTE — 9.2.1(2) NOTE — 10.6.1(3) NOTE — 10.6.2.2 Table 10.6 — 10.8(2) NOTE — 10.9.1(4) NOTE — 10.13(2) NOTE — A.3.2(1) NOTE — A.4(1) NOTE — A.4(3) NOTE 1 — A.4(3) NOTE 2 — A.4(4) NOTE — A.5(1) NOTE — E.3.1(2) NOTE — E.3.1(3) NOTE — H.2(6) NOTE — O.2(2) NOTE — S.8.4(1) NOTE

National choice is allowed in EN 1999-1-1 on the application of the following informative annexes: Annex B (Informative) Finite element Methods of analysis (FEM)

Annex C (Informative) Materials selection

Annex D (Informative) Corrosion and surface protection

Annex F (Informative) Analytical models for stress-strain relationship Annex G (Informative) Geometrical properties of cross-sections

Annex H (Informative) Behaviour of cross-sections beyond elastic limit

Annex I (Informative) Lateral torsional buckling of beams and torsional or torsional-flexural buckling of compressed members

Annex J (Informative) Shear lag effects in member design

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Annex L (Informative) Cross-sectional ductility and rotation capacity Annex M (Informative) Classification of joints

Annex N (Informative) The use of the component method for joints Annex O (Informative) Screw grooves

Annex P (Informative) Adhesive bonded joints

Annex Q (Informative) Determining the extent of HAZ from hardness tests Annex T (Informative) Lattice Spatial Roof Structures

Annex U (Informative) Composite Aluminium Concrete Beams

The National Annex can contain, directly or by reference, non-contradictory complementary information for ease of implementation, provided it does not alter any provisions of the Eurocodes.

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1 Scope

1.1 Scope of EN 1999-1-1

(1) This document gives basic design rules for structures made of wrought aluminium alloys and limited guidance for cast alloys (see Clause 5 and Annex C).

This document does not cover the following unless otherwise explicitly stated in this standard: — components with material thickness less than 0,6 mm;

— welded components with material thickness less than 1,5 mm; — connections with:

— steel bolts and pins with diameter less than 5 mm; — aluminium bolts and pins with diameter less than 8 mm;

— rivets and thread forming screws with diameter less than 3,9 mm.

1.2 Assumptions

(1) In addition to the general assumptions of EN 1990 the following assumptions apply: — execution complies with EN 1090-3;

— the aluminium products comply with EN 573 and the products listed in 2.3.

— the mechanical properties comply with the tabulated values in Parts 2 of the product standards listed in 2.3.

(2) EN 1999 is intended to be used in conjunction with:

— European Standards for construction products relevant for aluminium structures

— EN 1090-1, Execution of steel structures and aluminium structures – Part 1: Requirements for conformity assessment of structural components

— EN 1090-3, Execution of steel structures and aluminium structures – Part 3: Technical requirements for aluminium structures

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2 Normative references

The following documents are referred to in the text in such a way that some or all of their content constitutes requirements of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies.

NOTE See the Bibliography for a list of other documents cited that are not normative references, including those referenced as recommendations (i.e. through ‘should’ clauses) and permissions (i.e. through ‘may’ clauses).

prEN 1990:2020, Eurocode - Basis of structural and geotechnical design EN 10204, Metallic products - Types of inspection documents

EN 1991-2, Eurocode 1: Actions on structures - Part 2: Traffic loads on bridges

EN 1999-1-3, Eurocode 9: Design of aluminium structures - Part 1-3: Structures susceptible to fatigue EN 1993-1-8, Eurocode 3: Design of steel structures - Part 1-8: Design of joints

EN 1993-1-11, Eurocode 3 - Design of steel structures - Part 1-11: Design of structures with tension components

EN ISO 13918, Welding - Studs and ceramic ferrules for arc stud welding (ISO 13918)

3 Terms, definitions and symbols

3.1 Terms and definitions

For the purposes of this document, the terms and definitions given in EN 1990 and the following apply. 3.1.1

frame

whole of or a portion of a structure, comprising an assembly of directly connected structural members, designed to act together to resist load; this term refers to both moment-resisting frames and triangulated frames; it covers both plane frames and spatial frames

3.1.2 sub-frame

frame that is part of a larger frame, but is treated as an isolated frame in a structural analysis 3.1.3

connection

location at which two members are interconnected and assembly of connection elements and - in case of a major axis joint - the load introduction into the column web panel

Note 1 to entry: A “connection” is the system, which mechanically fastens a given member to the remaining part of the structure. It should be distinguished from the term "joint", which usually means the system composed by the connection itself plus the corresponding interaction zone between the connected members (see Figure M.1).

3.1.4 joint

assembly of basic components that enables members to be connected together in such a way that the relevant internal forces and moment can be transferred between them

Note 1 to entry: A beam-to-column joint consists of a web panel and either one connection (single sided joint configuration) or two connections (double sided joint configuration).

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3.1.5

semi-continuous joint

joint in which the structural properties of the members and connections need explicit consideration in the global analysis

3.1.6

continuous joint

joint in which only the structural properties of the members need be considered in the global analysis 3.1.7

simple joint

joint that is not required to resist moments 3.1.8

global analysis

determination of a consistent set of internal forces and moments in a structure, which are in equilibrium with a particular set of actions on the structure

3.1.9

system length

distance in a given plane between two adjacent points at which a member is braced against lateral displacement, or between one such point and the end of the member

3.1.10

buckling length

length of an equivalent uniform member with pinned ends, which has the same cross-section and the same elastic critical force as the verified uniform member (individual or as a component of a frame structure)

3.1.11

shear lag effect

non-uniform stress distribution in wide flanges due to shear deformations; it is taken into account by using a reduced “effective” flange width in safety assessments

3.1.12

capacity design

design based on the plastic deformation capacity of a member and its connections providing additional strength in its connections and in other parts connected to the member

3.1.13 open section

type of section prone to torsional or lateral-torsional buckling, e.g. I-, H-, U-, Z-, C-sections with low torsional stiffness

Note 1 to entry: The section can include small hollow parts, but still stability needs to be verified.

Note 2 to entry: The design provisions in this standard distinguish between open section, closed/hollow section and solid section, see Table 3.1.

3.1.14

closed/hollow section

type of section such as rectangular and square hollow sections (RHS, SHS), circular hollow sections (CHS) but also complicated hollow sections with outstands, i.e. sections with large torsional stiffness so that lateral-torsional buckling is not decisive

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3.1.15 solid section

type of section of rod or bar or other compact sections that may have small hollow parts and small compact outstand parts

Table 3.1 — Examples of cross-sections a

EN 1999-1-1 Open Closed/Hollow b _Solid

Cross-section

EN 12258 Solid Hollow Hollow Solid Hollow

a _{To avoid misunderstanding between the design engineer and the manufacturer/provider of extruded sections, one}

should be aware that according to EN 12258 (Aluminium – terms and definitions) differing terms for semi products are used. One distinguishes there between

⎯ Hollow section profile in which the cross-section completely encloses one or more voids; ⎯ Solid section profile in which the cross-section does not include any enclosed void.

b _{The section may be considered as closed if the distance between the webs is larger than one third of the section}

height.

3.2 Symbols

For the purposes of this document, the following symbols apply.

NOTE Additional symbols are defined where they first occur.

Latin upper-case letters

8 gross cross-section

A _{= 𝐴}

5,65√𝐴0 , elongation value measured with a reference length, 5,65 √𝐴0, see EN ISO 6892

A_ch cross-sectional area of one chord of a built-up column A_d area of one diagonal of a built-up column

A_e the section area of an un-welded section, and the effective section area obtained by taking a reduced thickness, ρ_o,haz, for the HAZ material of a welded section

A_eff effective cross-section area A_f area of the tension flange

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A_f,net net area in the section with fastener holes A_f1, A_f2 cross-section area of top and bottom flange A_fc cross-section area of compression flange A_g gross cross-section area

A_net net cross-section area A_nt net area subject to tension A_nv net area subject to shear A_s tensile stress area of a bolt

A_st area of all longitudinal stiffeners within half the flange width A_st,eff effective area of the stiffener column, see Figure 8.29(c)

A_u,eff effective cross-section area allowing for local buckling and HAZ softening of transverse welds

A_v shear area

A_v area of one post (or transverse element) of a built-up column A_w cross-section area of web

A₀ cross-section area of the hole

A₁ area of part of angle outside the bolt hole

A₅₀ elongation value measured with a constant reference length of 50 mm, see EN ISO 6892

BC buckling class

B_Ed design value of bimoment

B_o conventional bolt strength at elastic limit B_p,Rd design punching shear resistance per bolt

B_t,Rd design tension resistance of a bolt-plate assembly B_u,Rd tension resistance of a bolt-plate assembly

B_x bending stiffness of orthotropic plate in section x = constant B_y bending stiffness of orthotropic plate in section y = constant

C_o reduction factor for ρ_o,haz, depending of the thickness, the filler material and the welding process

C_u reduction factor for ρ_u,haz, depending of the thickness, the filler material and the welding process

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C₁, C₂ constants C₁, C₂, C₃,

C_1,0, C_1,1

factors in formulae for relative critical moment

D diameter of circle inscribed in fillet or bulb D_m diameter to mid-thickness of round tube E modulus of elasticity

E_k characteristic value of action effect F load, generalised force

F_o,Rd design value of pull-out resistance

F_v,Rd contact resistance against shear forces of the screw acting perpendicular to the channel

F_w,Rd design weld resistance per length F_w,Rd design value of the weld force per length F_b,Rd design bearing resistance per bolt

F_cr elastic critical buckling load for global instability mode based on initial elastic stiffness F_e elastic load, elastic generalised force

F_Ed design value of loading (design load) on the structure F_Ed design value of transverse force

F_p,A preloading force

F_Rd design resistance to transverse force

F_s,Rd design slip resistance per bolt at the ultimate limit state F_s,Rd,ser design slip resistance per bolt at the serviceability limit state F_t,Ed design value of tensile force per bolt for the ultimate limit state

F_tt,Rd design value of tensile resistance of the screw groove and port at the section through the tip of the screw

F_t,Rd design tension resistance per bolt

F_tb,Rd design tensile resistance of the fusion zone

F_tb,Rk characteristic tensile resistance of the fusion zone F_u ultimate load, ultimate generalised force

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F_v,Ed design value of shear force per bolt for the ultimate limit state F_v,Ed,ser design value of shear force per bolt for the serviceability limit state

F_v,Rd design value of shear resistance of the screw for loads within 0° ≤ θ ≤ 180° towards the opening of the groove

F_v,Rd design shear resistance per bolt

F_vp,Rd design value of shear resistance of the screw for loads within -60° ≤ θ ≤ -120° (opposite the opening of the groove)

G shear modulus

G_k nominal value of the effect of permanent actions H torsional stiffness of orthotropic plate

HAZ heat affected zone

H_Ed design value of the horizontal reaction at the bottom of the storey to the horizontal loads and fictitious horizontal loads

I_b in plane second moment of area of a batten I_ch in plane second moment of area of a chord

I_eff effective second moment of area of the built-up member

I_eff second moment of area of effective cross-section of plating for in-plane bending I_eff second moment of area for the effective cross-section for the ultimate limit state, with

allowance for local buckling

I_ep second moment of area of the end-post section about the centre-line of the web I_fc second moment of area of the compression flange about the minor axis of the section I_ft second moment of area of the tension flange about the minor axis of the section I_gr second moment of area of the gross cross-section

I_L second moment of area of one stiffener and adjacent plating in the longitudinal direction

I_s second moment of area about the minor axis

I_ser second moment of area for the effective cross-section for the serviceability limit state I_sl second moment of area of the stiffener closest to the loaded flange

I_st second moment of area of gross cross-section of stiffener and adjacent effective part of the web about an axis through its centroid and parallel to the plane of the web

I_t torsion constant I_w warping constant

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L member length

L_cr buckling length in the buckling plane considered L_b,e bolt elongation length

L_b length of the perimeter of the head of the bolt in contact with the side section of the channel in bolt-channel joints

L_e embedded length in screw joints, which is the screw length with threads fully in the aluminium slot

L_ch buckling length of chord

L_cr,z buckling length for lateral torsional buckling

L_Ed design value of the component of the force, F_w,Ed, in the direction of the weld axis L_eff effective length for resistance to transverse force

L_j distance between the centres of the end fasteners in a long joint L_n total screw length within the groove

L_o original gauge length L_p screw point length

L_w total length of longitudinal fillet weld L_w,eff effective length of longitudinal fillet weld

l_y effective loaded length for resistance to transverse force M_cr elastic critical moment for lateral-torsional buckling

M_Ed design value of the maximum moment in the middle of the built-up member considering second order effects

𝑀EdI design value of the maximum moment in the middle of the built-up member without second order effects

M_Rd design bending moment resistance for actual cross-section class M_b,Rd design moment resistance for lateral-torsional buckling

M_Ed design value of bending moment

M_f,Rd design moment resistance of a cross-section consisting of the flanges only M_N,Rd reduced design moment resistance due to presence of axial force

M_o elastic bending moment corresponding to the attainment of the proof stress, f_o M_o,Rd design resistance for bending moment to general yielding

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M_Rk characteristic moment resistance of the critical cross-section

M_u,Rd design resistance for bending moment of the net cross-section at holes

M_V,Rd reduced design bending resistance making allowance for the presence of shear force M_y,Ed design value of bending moment, y-y axis

M_y,Rd design bending moment resistance about y-y axis M_z,Ed design value of bending moment, z-z axis

M_z,Rd design bending moment resistance about z-z axis

N_u,Rd design resistance for uniform compression in sections with transverse weld N_b,Rd design buckling resistance of a compression member or chord

N_c,Rd design resistance for uniform compression of the cross-section

N_ch,Ed design value of compression force in the chord at mid-length of the built-up member N_cr elastic critical force for the relevant buckling mode based on the gross cross-sectional

properties N_cr,y,

N_cr,z, N_cr,T

elastic flexural buckling load (y-y and z-z axes) and torsional buckling load

N_Ed design value of the axial force

N_net,Rd design resistance of section at bolt holes

N_o,Rd design resistance to general yielding of a member in tensions N_Rd design resistance to normal force

N_Rk characteristic resistance to normal force of the critical cross-section N_t,Rd design resistance to tension force

N_u,Rd design resistance to axial force of the net cross-section at holes for fasteners P_k nominal value of the effect of prestressing imposed during erection

Q prying force

R_d design value of resistance

R_e,Ed reaction at the end of the girder under design loading

R_Ed design value of the resultant of the components of the force, F_w,Ed, in the weld seam cross-section

R_k characteristic value of resistance S position of shear centre

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S_v shear stiffness of the lacings or battened panel of built-up member T highest temperature the structure is operating

T_Ed design value of torsional moment

T_Rd design St. Venant's torsion moment resistance

T_t,Ed design value of internal St. Venant's torsional moment T_w,Ed design value of internal warping torsional moment T₁ interpass temperature

U utilization grade

U(x_s) utilization grade in the section of the splice or connection

V_Ed total design value of vertical load on the structure on the bottom of the storey V_Ed design value of shear force

V_eff,1,Rd design block tearing resistance for concentric loading V_eff,2,Rd design block tearing resistance for eccentric loading V_f,Rd design shear resistance contribution from the flanges V_Rd design shear resistance of cross-section

V_T,Rd reduced design shear resistance making allowance for the presence of torsional moment

V_w,Rd design shear resistance contribution from the web W_Ed total design loading on the adjacent span

W_eff effective elastic section modulus, obtained using a reduced thickness, t_eff, or the class 4 parts

W_eff,haz effective elastic section modulus, obtained using a reduced thickness, ρ_ct, for the class 4 parts or a reduced thickness, ρ_o,hazt, for the HAZ material, whichever is the smaller W_el elastic modulus of the gross cross-section (see 8.2.5.2)

W_el,haz effective elastic modulus of the gross cross-section, obtained using a reduced thickness, ρ_o,hazt, for the HAZ material

W_net elastic modulus of the net section allowing for holes and HAZ softening, if welded W_pl plastic modulus of gross cross-section

W_pl,haz effective plastic modulus of the gross cross-section, obtained using a reduced thickness, for the HAZ material

W_T,pl plastic torsion modulus o,hazt 

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W_u,eff section modulus allowing for local buckling and reduced thickness, ρ_u,hazt, in HAZ softening of transverse welds

X, Y coefficients for calculation of relative slenderness for lateral-torsional buckling X_k characteristic value of a strength property of a material

X_kT characteristic strength value for the material at temperature between 80 °C and 100 °C X_n nominal value of material property

Latin lower-case letters

a effective throat thickness

a_c half-wavelength for elastic buckling of stiffener a_d design value of geometrical data

apen weld penetration

a_pin, b_pin plate thickness in a pin connection a_st, b_st, c_st coefficients in formula for η_st

a_st,1 relative area of stiffeners, area of stiffeners divided by centre to centre distance of stiffeners

a₀, a₁, a₂, a₃, a_max

widths of corrugations

b width of cross-section part b_eff effective width for shear lag b_f, b₁, b₂ flange widths

b_haz extent of HAZ

b_sh width of a flat cross-section part b_w distance between weld toes of flanges

b₀ width of outstand or half width of internal cross-section part

b₁ depth of the loaded sub-panel taken as the clear distance between the loaded flange and the stiffener

c depth of the rib or lip c_e elastic support from plate c_f factor in formula for V_f,Rd d diameter of a fastener

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d_ch distance along a chord of a built-up member between two consecutive lacings or battens

d_m mean of the across points and across flats dimensions of the bolt head or the nut or if washers are used the outer diameter of the washer, whichever is smaller

d_sl internal diameter of a groove d₀ diameter of hole

e centre to centre distance between stiffeners e_e effective edge distance

e_min minimum edge distance

e_w weld spacing in intermittent welds

e₀ maximum amplitude of the initial bow imperfection

e_0,d design value of maximum amplitude of the initial bow imperfection e₁, e₄ edge distances

f_o characteristic value of 0,2 % proof strength

f_o,haz characteristic value of 0,2 % proof strength in heat affected zone, HAZ f_o,V reduced design strength making allowance for the presence of shear force f_oc characteristic value of 0,2 % proof strength of cast material

f_of characteristic value of 0,2 % proof strength of flange material f_ow characteristic value of 0,2 % proof strength of web material f_u characteristic value of ultimate tensile strength

f_u,haz characteristic value of ultimate tensile strength in heat affected zone, HAZ f_ub characteristic ultimate strength of bolt material or of the weld stud material

f_ub,haz characteristic value of ultimate tensile strength in heat affected zone of the weld stud f_uc characteristic value of ultimate tensile strength of cast material

f_ur characteristic ultimate strength of rivet material f_v,adh characteristic shear strength values of adhesives f_uw characteristic ultimate strength of web material f_v,haz characteristic shear strength in HAZ

f_w characteristic strength of the weld metal f_w0 0,2 % proof strength of the weld metal

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f_wv,d design shear strength of the weld g distance from weld toe to centre of bolt

g_c width of the opening of the channel in bolt channel joints h storey height, height of the structure

h_f distance between centres of flanges

h_s distance between shear centre of upper flange and shear centre of bottom flange h_w web depth = clear distance between flanges

h₀ distance between the centroids of chords of a built-up column

i radius of gyration about the relevant axis, determined using the properties of the gross cross-section

i_min minimum radius of gyration of one chord or one angle i_s polar radius of gyration

i_y, i_s, i₀ radius of gyration (y-y axis, z-z axis and 0-0 axis) i_z minor axis radius of gyration of the gross cross-section k buckling length factor

k_F buckling factor for transverse force

k_g coefficient which is depending on the shear strength of the threads in screw-groove joints

k_s reduction factor for slip resistance of a preloaded bolt depending on connection configuration

k_w end condition corresponding to rotation about the longitudinal axis

k_y end condition corresponding to restraints against movement in plane of loading k_z end condition corresponding to restraints against lateral movement

k_τ buckling coefficient for shear buckling

k_τ,st contribution from the longitudinal stiffeners to the buckling coefficient k_τ1 buckling coefficient for sub panel

k₁ coefficient for bolt-channel joints

k₁₀₀ coefficient for reduction of a strength property of a material at temperature between 80 °C and 100 °C

k₂ factor for tension resistance of a bolt k2 coefficient for bolt-channel joints

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l_e parameter in formulae for effective loaded length l_eff effective length

l_w half wave-length in elastic buckling m number of columns in a row m, k numerical parameters m_x,Rd,

m_y,Rd

design bending moment resistances based on stresses in the plate

m₁, m₂ parameters in formulae for effective loaded length n number of friction interfaces

n_p exponent in Ramberg-Osgood formula for plastic design

p spacing of the centres of the same two holes measured perpendicular to the member axis

p_th threaded parts of the periphery inside the hole or groove p, p₁, p₂ spacing between bolt holes

q_0,d design value of equivalent force per length r radius of curvature

s staggered pitch, the spacing of the centres of two consecutive holes in the chain measured parallel to the member axis

s, X coefficients to calculate λ_t

s_d developed width of stiffeners and adjacent plate s_e loaded length in section between flange and web s_s length stiff bearing under transverse force t thickness of a cross-section part

te deep penetration throat thickness, i.e. nominal or effective throat thickness to which a _{certain amount of fusion penetration is added} t_f flange thickness

t_p thickness of the plate under the bolt head or the nut t_pl mean value of adjacent material thickness

t_sup thickness of the upper flanges of the cannel in bolt channel joints

t_sb minimum thickness of the side wall of the channel (tlat) and thickness of the bottom wall of the channel (tinf) in bolt channel joints

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t_w web thickness

t₁, t₂ thickness of layers or flanges

u - u major principal axis (where this does not coincide with the y-y axis) v generalised deformation

v - v minor principal axis (where this does not coincide with the z-z axis) v_e deformation corresponding to elastic generalised force

v_u deformation corresponding to ultimate generalised force v₁ reduction factor for shear bucklingx – x axis along a member

x_s,haz distance from the localised weld to a support or point of contra flexure for the deflection curve for elastic buckling from axial force only

x_s distance from the splice or end connection to the nearest point of contra-flexure for the deformation curve for elastic buckling

y - y axis of a cross-section

y_st distance from centre of plating to centre of outermost stiffener z - z axis of a cross-section

z_a coordinate of the load application point related to centroid z_g coordinate of the load application point related to shear centre z_j mono-symmetry constant

z_s coordinate of the shear centre related to centroid

z₁ distance from neutral axis to most severely stressed fibre (along the z-z axis) z₂ distance from neutral axis to fibre under consideration (along the z-z axis) α fillet or bulb factor; angle between flat section parts adjacent to fillets α, α_y, α_z shape factor

α factor for the calculation of effective length for stiffened flanges _b, k₁ factors for bearing resistance of the connected parts

α_cr factor by which the design loads would have to be increased to cause elastic instability in a global mode

α_h reduction factor for height h applicable to columns α_i imperfection factor

α_LT imperfection factor

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α_M,j correction factor for ultimate bending moment depending on the different behavioural classes of cross-sections

α_M,red correction factor for welded class 1 cross-section

α_N,j correction factor for ultimate axial load depending on the different behavioural classes of cross-sections

α_T coefficient of linear thermal expansion

α_u load magnification factor (to the ultimate limit state) α_v factor for shear resistance of a bolt

α_yw, α_zw coefficients in formulae for torsional and torsional-flexural buckling α_ξ shape factor α₅ or α₁₀

α₀ geometrical shape factor α₂ factor for b_haz

α_3,u shape factor for class 3 cross-section without welds α_3,w shape factor for class 3 cross-section with welds

α₅, α₁₀ generalized shape factors corresponding to ultimate curvaturevalues, χ_u = 5χ_el and χ_u = 10χ_el

β width-to-thickness ratio, b/t β, δ, γ fillet or bulb factors

β_Lf reduction factor for long joint

_p reduction factor for fasteners passing through packings β_s effective width factor for shear lag

β₁, β₂, β₃ limits for slenderness parameter

₂, ₃ reduction factors for connections of angles

γ

_M global partial factor

γ

_M1 factor for resistance of cross-sections and resistance of members to instability (based on f_o)

γ

_M2 partial factor for resistance of cross-sections to fracture

γ

_Ma partial factor for resistance of adhesive bonded connection

γ

_Mf partial factor for fatigue

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γ

_Ms,ser partial factor for slip resistance at serviceability limit state

γ

_Ms partial factor for slip resistance

γ

_Mw partial factor for resistance of welded connection

γ

_Mw partial factor for welded joints

γ

_Ms relative second moment of area of the stiffener closest to the loaded flange

δ_H,Ed horizontal displacement at the top of the storey, relative to the bottom of the storey δ_q in-plane deflection of a bracing system

ε _{√250 𝑓}_⁄ _o_{, f}_o_{in N/mm}2_{, factor}

_true true strain

_u characteristic value of elongation at rupture A ζ_g relative coordinate of the point of load application ζ_j relative cross-section mono-symmetry parameter

η coefficient to allow for stress gradient or stiffening of cross-section part

η_ep correction factor depending on geometrical shape factor and conventional available ductility of the material

η_sb factor for shear buckling resistance in plastic range η_v factor for shear area

η_y0, η_z0, β_z0, ψ

exponents in interaction formulae for bending and compression

η_y, η_z, β_z, ψ_c

exponents in interaction formulae for buckling due to bending and compression

η_cr shape of the elastic critical buckling mode θ angle between axes of chord and lacings

θ_p, θ_el, θ_u plastic rotation, elastic rotation and maximum plastic rotation corresponding to ultimate curvature χ_u

κ notional width-to-length ratio for flange κ_wt relative torsion parameter

𝜆̅ relative slenderness

𝜆̅c,1 relative slenderness for local buckling 𝜆̅c,g relative slenderness for global buckling

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𝜆̅haz, 𝜆̅haz,LT

relative slendernesss for section with localised weld

𝜆̅LT relative slenderness for lateral-torsional buckling λ_t coefficients in formula for relative slenderness, 𝜆̅_T

relative slenderness for torsional and torsional-flexural buckling 𝜆̅T relative slenderness for torsional or torsional-flexural buckling 𝜆̅w relative slenderness for shear buckling

λ₀ coefficients to calculate λ_t

𝜆̅0 length of the horizontal plateau of the buckling curves

𝜆̅0,LT length of horizontal plateau of lateral torsional buckling curves μ slip factor, efficiency factor

μ_cr relative critical moment ν Poisson’s ratio in elastic range ξ ductility factor

ρ unit mass

ρ_c,1 reduction factor for local buckling ρ_c,g reduction factor for global buckling ρ_c reduction factor for local buckling

ρ_o,haz = f_o,haz/f_o ratio between 0,2 % proof strength in HAZ and in parent material ρ_u,haz = f_u,haz/f_u ratio between ultimate strength in HAZ and in parent material

ρ_v reduction factor to determine reduced design value of the resistance to bending moment making allowance of the presence of shear force

ρ_v factor for shear buckling resistance

σ_cr elastic critical stress for a stiffened cross-section part σ_cr0 elastic critical stress for an un-stiffened cross-section part σ_eq,Ed equivalent design stress for castings

σ_gr maximum compressive bending stress at the serviceability limit state based on the gross cross-section

σhaz,Ed design value of normal stress in HAZ, perpendicular to the weld axis σ_Rd design resistance for castings

_true true stress T

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_w,Ed design value of normal stress due to the bimoment BEd σ_x,Ed design value of stress in x-x axis direction for castings σ_x,Ed design value of the local longitudinal stress

σ_y,Ed design value of stress in y-y axis direction for castings σ_y,Ed design value of the local transverse stress

σ_⊥ normal stress perpendicular to weld axis σ_|| normal stress parallel to weld axis

τ average shear stress in the adhesive layer τ_|| shear stress parallel to weld axis

τ_cr,1 shear buckling stress for local buckling τ_cr,g shear buckling stress for orthotropic plate τ_cr,g shear buckling stress for global buckling τ_Ed design value of the local shear stress τ_haz,Ed design value of shear stress in HAZ

τ_t,Ed design value of shear stress due to St. Venant's torsion τ_w,Ed design value of shear stress due to warping torsion τ_xy,Ed design value of shear stress for castings

τ_⊥ shear stress perpendicular to weld axis φ value to determine the reduction factor, χ φ global initial sway imperfection

ϕ, η_h factors

ϕ_LT value to determine the reduction factor, χ_LT ₀ basic value for global initial sway imperfection χ reduction factor for relevant buckling mode χ_el elastic bending curvature (= χ_0,2)

χ_F reduction factor for local buckling due to transverse force

χ_LT,haz reduction factor for lateral-torsional buckling of the beam in a cection with HAZ χ_LT reduction factor for lateral-torsional buckling of the beam

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ψ stress ratio

ψ_f mono-symmetry factor ω_x,haz,

ω_x,LT,haz

factors for section with localised transverse weld

ω_x, ω_x,LT factors for second order bending moments

NOTE 1 Notations for models for stress-strain relationship are given in Annex F. NOTE 2 Notations for cross-section constants are given in Annex G, G.4, G.5 and G.6.

3.3 Conventions for member axes

(1) In general, the convention for member axes is: x-x - along the member

y-y - axis of the cross-section z-z - axis of the cross-section

(2) For aluminium members, the conventions used for cross-section axes are: — generally:

y-y - cross-section axis parallel to the flanges z-z - cross-section axis perpendicular to the flanges — for angle sections:

y-y - axis parallel to the smaller leg z-z - axis perpendicular to the smaller leg — where necessary:

u-u - major principal axis (where this does not coincide with the y-y axis) v-v - minor principal axis (where this does not coincide with the z-z axis) (3) The symbols used for axes of aluminium sections are indicated in Figure 3.1.

(4) The convention used for subscripts, which indicate axes for moments is: "Use the axis about which the moment acts."

NOTE All rules in this Eurocode relate to principal axis properties, which are generally defined by the axes y-y and z-z for symmetrical sections and by the u-u and v-v axis for unsymmetrical section such as angles.

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Figure 3.1 — Definition of axes for various cross-sections y z y z y z y z y z y z z z y y z v z y y v u u y z z y z z y y z z y y z z y y y y z z z z y y y z y z y z y z z y z z y y _{y y} z z y y z z z z y y z z y y u u v v z y 2 1 3 3 y z z y 1) 1)

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4 Basis of design

4.1 General rules

Basic requirements

(1) The design of aluminium structures shall be in accordance with the general rules given in EN 1990. (2) The supplementary provisions for aluminium structures in this clause shall also be applied.

(3) The basic requirements of Clause 4 should be deemed to be satisfied where limit state design is used in conjunction with the partial factor method and the load combinations given in EN 1990 together with the actions given in EN 1991.

(4) The rules for resistances, serviceability and durability given in the various parts of EN 1999 should be applied.

(5) Supplemental requirements in Annex S to those given in the main part of this standard shall be applied for the structural design of bridges.

Structural reliability

(1) Where different levels of reliability are required, these levels should be achieved by an appropriate choice of quality management measures in design and execution, according to EN 1990, EN 1090-3 and Annex A.

(2) Aluminium structures and components should be classified by execution classes in accordance with Annex A.

(3) The execution should be carried out in accordance with EN 1090-1 and EN 1090-3. The information, which EN 1090-3 requires to be included in the execution specification, should be provided.

NOTE Options to be specified according to EN 1090-3 can be set by the National Annex for the reliability levels.

Design service life, durability and robustness

(1) Depending on the type of action affecting durability and the design service life (see EN 1990) aluminium structures should be

— designed for corrosion (see Clause 6);

— designed for sufficient fatigue life (see EN 1999-1-3); — designed for wearing;

— designed for accidental actions (see EN 1991-1-7); — specified for inspection and maintenance.

NOTE 1 Guidance on the design for corrosion is given in Annex C and Annex D. NOTE 2 Requirements for fatigue are given in EN 1999-1-3.

4.2 Principles of limit state design

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(2) The resistances specified in this document may be used where the conditions for materials in Clause 5 are met.

4.3 Basic variables

Actions and environmental influences

(1) Actions for the design of aluminium structures should be in accordance with EN 1991. For the combination of actions and partial factors of actions, see EN 1990.

(2) The actions to be considered during execution should be obtained from EN 1991-1-6.

(3) Where the effects of predicted absolute and differential settlements need be considered the best estimates of these imposed deformations should be used.

(4) The effects of uneven settlements, imposed deformations or other forms of prestressing imposed during execution should be taken into account by their characteristic value and combined with other actions in accordance with EN 1990.

(5) Fatigue loading not defined in EN 1991 should be determined in accordance with EN 1999-1-3. Material and product properties

(1) Material properties for aluminium construction products should be in accordance with clause 5.

4.4 Verification by the partial factor method

Design value of material properties

(1) For the design of aluminium structures characteristic values x_k or nominal values x_n of material properties shall be used as indicated in this Eurocode.

Design value of geometrical data

(1) Geometrical data for cross-sections and systems may be taken from product standards or drawings for the execution according to EN 1090-3 and treated as nominal values.

(2) Design values of equivalent geometrical imperfections specified in this standard comprise

— the effects of geometrical imperfections of members as governed by geometrical tolerances in product standards or the execution standard;

— the effects of structural imperfections from fabrication and erection, residual stresses, variations of the yield strength and heat-affected zones.

Design resistances

(1) For aluminium structures Formula (4.1) applies:

R_d = R_k/_M (4.1)

where

R_k is the characteristic value of the resistance of a cross-section or member determined with characteristic or nominal values for the material properties and cross-sectional dimensions;