Seismic Design Philosophy (EN 1998-1 Cl. 2.1)
- No-collapse requirement (ULS): Structure must sustain the design seismic action without local or global collapse.
- Damage limitation requirement (SLS): Structure must withstand a more frequent seismic action without damage.
For ordinary buildings (Importance Class II), the reference return period for the no-collapse requirement is 475 years (10% probability of exceedance in 50 years).
Importance Classes (EN 1998-1 Cl. 4.2.5)
| Importance Class | Building Type | (\gamma_I) |
|---|---|---|
| I | Minor buildings, agricultural sheds, temporary structures | 0.80 |
| II | Ordinary buildings — residential, commercial, office | 1.00 |
| III | Schools, assembly halls, cultural institutions | 1.20 |
| IV | Hospitals, fire stations, power plants | 1.40 |
Design ground acceleration: (ag = \gamma_I \times a{gR}), where (a_{gR}) is the reference peak ground acceleration on Type A ground.
Ground Types and Spectral Parameters
| Ground Type | Description | vs,30 (m/s) | S (Soil Factor) | TB (s) | TC (s) | TD (s) |
|---|---|---|---|---|---|---|
| A | Rock or rock-like formation | > 800 | 1.00 | 0.15 | 0.40 | 2.00 |
| B | Very dense sand, gravel, stiff clay | 360-800 | 1.20 | 0.15 | 0.50 | 2.00 |
| C | Medium-dense sand, gravel, stiff clay | 180-360 | 1.15 | 0.20 | 0.60 | 2.00 |
| D | Loose-to-medium cohesionless or soft soil | < 180 | 1.35 | 0.20 | 0.80 | 2.00 |
| E | Surface alluvium over stiffer material | — | 1.40 | 0.15 | 0.50 | 2.00 |
Type 1 Elastic Response Spectrum
For 0 âÃÂä T âÃÂä TB: (S_e(T) = a_g \times S \times [1 + T/T_B \times (\eta \times 2.5 - 1)]) For TB âÃÂä T âÃÂä TC: (S_e(T) = a_g \times S \times \eta \times 2.5) For TC âÃÂä T âÃÂä TD: (S_e(T) = a_g \times S \times \eta \times 2.5 \times [T_C / T]) For TD âÃÂä T âÃÂä 4.0s: (S_e(T) = a_g \times S \times \eta \times 2.5 \times [T_C \times T_D / T^2])
Where ÃÂ÷ = âÃÂÃÂ[10/(5+ÃÂþ)] âÃÂÃÂ¥ 0.55 (for 5% damping in steel structures, ÃÂþ = 5 âÃÂàÃÂ÷ = 1.0).
Behaviour Factors q for Steel Structures (EN 1998-1 Cl. 6.3)
The behaviour factor q reduces the elastic seismic force demand to a design-level force, reflecting ductility and energy dissipation capacity. Higher q means lower design forces but more stringent ductility detailing.
[ q = q_0 \times k_w \geq 1.5 ]
Behaviour Factors — Moment-Resisting Frames (MRF)
| Ductility Class | q0 | Multiplier | Maximum q | Application |
|---|---|---|---|---|
| DCL | âÃÂä 1.5 | None | 1.5 | Non-dissipative, elastic design |
| DCM | 4.0 | ÃÂñu/ÃÂñ1 | 5.2 | Standard mid-rise frames |
| DCH | 5.0 | ÃÂñu/ÃÂñ1 | 6.5 | High-seismicity, stringent detailing |
Behaviour Factors — Braced Frames
| Structural Type | Ductility Class | q0 | Max q | Key Limitation |
|---|---|---|---|---|
| CBF — Diagonal bracing | DCM | 3.0 | — | Brace buckling in compression |
| CBF — Diagonal bracing | DCH | 4.0 | 4.8 | Class 1 sections required |
| CBF — V-bracing (chevron) | DCM | 2.0 | 2.5 | Beam must resist unbalanced force |
| CBF — V-bracing (chevron) | DCH | 2.5 | 3.0 | Beam designed for brace overstrength |
| EBF | DCM | 4.0 | 5.0 | Links dissipate energy |
| EBF | DCH | 5.0 | 6.5 | Compact links with stiffeners |
| Inverted Pendulum | DCM/DCH | 2.0 ÃÂÃÂ kw | 2.0 | Limited energy dissipation |
Steel Material Requirements for Ductility
DCM — Dissipative Elements
| Property | Requirement | Purpose |
|---|---|---|
| fy,max / fy | âÃÂä 1.25 | Prevents premature yielding in adjacent members |
| fu / fy | âÃÂÃÂ¥ 1.10 | Strain-hardening capacity beyond yield |
| ÃÂõu (elongation at failure) | âÃÂÃÂ¥ 15% | Deformation capacity for cyclic plastic straining |
| Section class | Class 1 or 2 | Plastic hinge development |
DCH — Additional Requirements
| Property | DCM | DCH |
|---|---|---|
| ÃÂõu | âÃÂÃÂ¥ 15% | âÃÂÃÂ¥ 20% (open), âÃÂÃÂ¥ 15% (hollow) |
| Section class | Class 1 or 2 | Class 1 mandatory for plastic hinges |
| Connection certification | By calculation | Qualification testing required |
Capacity Design Principles
Weak beam / strong column (MRF): [ \Sigma M*{Rc} \geq 1.3 \times \Sigma M*{Rb} ]
Column design from overstrength: [ M*{Ed,column} = M*{Ed,G} + 1.1 \times \gamma*{ov} \times \Omega \times M*{Ed,E} ]
Where (\gamma*{ov} = 1.25) (material overstrength factor) and (\Omega = \min(M*{pl,Rd,i} / M_{Ed,i})) across all dissipative zones.
CBF brace connection design: [ N*{connection} \geq 1.1 \times \gamma*{ov} \times N_{pl,Rd,brace} ]
Worked Example — 6-Storey Steel CBF Office Building
Building: 6 storeys, h = 3.5 m (H = 21 m), plan 30 m ÃÂÃÂ 20 m, 4 braced bays on perimeter. Site: agR = 0.25g (moderate European seismicity). Ground Type C. DCM CBF with diagonal bracing (q = 3.0). Importance Class II ((\gamma_I = 1.0)).
Step 1 — Seismic mass: Dead = 5.5 kN/mÃÂò, Imposed = 3.0 kN/mÃÂò (ÃÂÃÂ2 = 0.3). Floor area = 600 mÃÂò. Per floor: m = 600 ÃÂà(5.5 + 0.3 ÃÂà3.0) / 9.81 = 391 tonnes. Roof: m = 600 ÃÂà(5.0 + 0.3 ÃÂà1.5) / 9.81 = 333 tonnes. Total M = 5 ÃÂà391 + 333 = 2,288 tonnes.
Step 2 — Fundamental period: (T_1 = 0.075 \times H^{3/4} = 0.075 \times 21^{0.75} = 0.075 \times 10.05 = 0.75) s.
Step 3 — Design spectrum: Elastic spectrum at T1: (S_e(0.75) = a_g \times S \times \eta \times 2.5) = 0.25 (\times) 9.81 (\times) 1.15 (\times) 1.0 (\times) 2.5 = 7.04 m/sÃÂò
Design spectrum: (S_d(T_1) = 7.04 / 3.0 = 2.35) m/sÃÂò.
Step 4 — Base shear: (F_b = S_d(T_1) \times M \times \lambda = 2.35 \times 2,288 \times 0.85 = 4,570) kN.
Step 5 — Brace design: Per brace (8 braces at ground, angle âÃÂà45ÃÂð): (N_{Ed,E} = 4,570 / (8 \times \cos 45ÃÂð) = 808) kN. Select SHS 200 (\times) 200 (\times) 10.0 S355J2: Npl,Rd = 2,630 kN, Nb,Rd âÃÂà1,894 kN > 808 kN — OK.
Step 6 — Overstrength factor: (\Omega = N*{pl,Rd} / N*{Ed,E} = 2,630 / 808 = 3.25).
Step 7 — Column design (capacity): (N*{Ed,col} = N*{Ed,G} + 1.1 \times 1.25 \times 3.25 \times N_{Ed,E,column}) The high (\Omega) = 3.25 drives very large column forces — in practice, reduce brace size to bring (\Omega) closer to 1.5-2.0 for economical column design.
Drift Limits (EN 1998-1 Cl. 4.4.3.2)
| Building Type | Drift Limit (ULS) |
|---|---|
| Brittle non-structural elements fixed to structure | 0.5% of storey height |
| Ductile non-structural elements | 1.0% of storey height |
| Non-structural elements designed to accommodate drift | 1.5% of storey height |
Design Resources
- EN 1993 Steel Grades
- European Steel Properties
- EN 1993 Column Buckling
- EN 1993 Connection Design
- EN 1990 Load Combinations
- All European References
Frequently Asked Questions
What is the difference between DCL, DCM, and DCH in steel seismic design? DCL (Ductility Class Low, q âÃÂä 1.5) is non-dissipative — the structure is designed elastically with no special ductility provisions, appropriate for low seismicity (agR (\times) S < 0.10g). DCM (Medium, q up to 5.2 for MRF / 3.0 for CBF) requires capacity design with ÃÂóov = 1.25, fy,max/fy âÃÂä 1.25, and fu/fy âÃÂÃÂ¥ 1.10 — this is the standard class for most European buildings. DCH (High, q up to 6.5 for MRF / 4.8 for CBF) imposes stricter requirements including ÃÂõu âÃÂÃÂ¥ 20% for open sections, Class 1 sections mandatory for plastic hinges, and typically requires connection qualification testing.
When can I use q = 1.5 (non-dissipative design) instead of a higher q-factor? Use q âÃÂä 1.5 when: (1) agR (\times) S < 0.10g (low seismicity regions — seismic forces are modest), (2) the structure is highly irregular (EN 1998-1 requires q reduction for irregularity), or (3) the client specifies elastic design for critical infrastructure. The penalty is 2.5-4 times higher design base shear compared with DCM, driving substantially larger sections. For most European seismic regions (Italy, Greece, Romania, Turkey, Slovenia), DCM is the economic minimum.
How do I apply capacity design to a concentrically braced frame? Brace connections are designed for the maximum force the brace can deliver: Nconnection âÃÂÃÂ¥ 1.1 (\times) ÃÂóov (\times) Npl,Rd,brace. The dissipative braces yield in tension and may buckle in compression. Beams at V-braced bays must resist the full unbalanced vertical force after compression brace buckling — the beam is designed for Nbeam = Npl,Rd,tension (\times) sinÃÂø + 0.3 (\times) Npl,Rd,compression (\times) sinÃÂø. Columns are designed for NEd,col = NEd,G + 1.1 (\times) ÃÂóov (\times) ÃÂé (\times) NEd,E, where ÃÂé is the minimum overstrength ratio across all braces. The key economic driver: minimise brace sections to reduce ÃÂé and keep column sizes practical.
What magnification factor for P-Delta effects in steel MRF? The inter-storey drift sensitivity coefficient ÃÂø = Ptot (\times) dr / (Vtot (\times) h) per EN 1998-1 Cl. 4.4.2.2 determines P-Delta treatment. If ÃÂø âÃÂä 0.1: negligible, may be ignored. If 0.1 < ÃÂø âÃÂä 0.2: multiply seismic effects by 1/(1-ÃÂø) for all storeys. If ÃÂø > 0.2: full second-order analysis required. ÃÂø > 0.3 is not permitted — the structure must be stiffened. For a typical 6-storey steel MRF, ÃÂø is 0.06-0.12, giving modest amplification (1.06-1.14).
How does EN 1998 handle seismic design of steel connections? Connections in dissipative zones follow capacity design: Rd,connection âÃÂÃÂ¥ 1.1 (\times) ÃÂóov (\times) Rpl,Rd,member. For MRF beam-to-column connections in DCH, the welded connection must resist 1.1 (\times) 1.25 (\times) Mpl,Rd,beam (âÃÂÃÂ¥ 1.375 Mpl,Rd). For CBF brace connections, the connection resists 1.1 (\times) 1.25 (\times) Npl,Rd,brace. Bolted connections in dissipative zones must be preloaded (Category B or C slip-resistant to EN 1993-1-8). Full-penetration butt welds in dissipative zones require Charpy certification.
Reference only. Verify all values against the current edition of EN 1998-1:2004 and the applicable National Annex. Seismic design is a specialised discipline — all designs must be independently verified by a qualified structural engineer. Educational reference only.