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CHAPTER 1: INTRODUCTION part C

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1 CHAPTER 1: INTRODUCTION part C
BFC Structural Steel and Timber Design Assoc Prof Dr DYeoh

2 Course content Assoc Prof Dr DYeoh

3 Outline of this Lecture
Notations and symbols in EC3 Recap of common structural steel sections Local buckling Understanding failure modes Section classification Assoc Prof Dr DYeoh

4 Recognizing important notations and symbols used in EC3
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5 Section Assoc Prof Dr DYeoh

6 Elastic section modulus
Area Elastic section modulus Plastic section modulus Second moment of area major axis Second moment of area minor axis Assoc Prof Dr DYeoh

7 Subscripts Ed = design value of an effect eg: MEd = design bending moment NEd = axial force Rd = deign resistance eg: MRd = design resistance for bending NRd = resistance to axial force el = elastic property eg: Wel = elastic section modulus pl = plastic property eg: Wpl = plastic section modulus Assoc Prof Dr DYeoh

8 ULS – Equation 6.10 Assoc Prof Dr DYeoh

9 SLS Assoc Prof Dr DYeoh

10 Recap of common structural steel section
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11 Rolled and formed sections
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12 Built-up sections Assoc Prof Dr DYeoh

13 Cold rolled sections Assoc Prof Dr DYeoh

14 Local buckling failure
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15 Some basic knowledge when designing with structural steel
Structural steel members are made of thin elements These thin elements are slender, as a result causing local instabilities (known as local buckling in flange and web) even before achieving yield strength. As such, cross section classification is important to account for such local instabilities. Assoc Prof Dr DYeoh

16 Assoc Prof Dr DYeoh

17 Understanding failure modes
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18 Fundamental modes of failure in Universal Column under compression
Overall yielding in compression Overall buckling as a strut Local buckling in flange toes Assoc Prof Dr DYeoh

19 Overall yielding in compression
Fundamental modes of failure in Universal Beam under compression (UB as column) Overall yielding in compression Overall buckling as a strut (about minor axis) Local buckling in flange toes and web Assoc Prof Dr DYeoh

20 Fundamental modes of failure in Universal Beam under flexure (UB as beam)
Overall yielding in flexure Overall lateral / torsional buckling Local buckling in compression flange under high strains Local buckling in web UB in flexure behaves differently to UB in axial compression Assoc Prof Dr DYeoh

21 Section Classification
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22 What? CLASS 1 CLASS 2 CLASS 3 CLASS 4 Assoc Prof Dr DYeoh

23 What does it mean? Think of plasticity Think of ductility
Think of rotational capacity in the whole section Assoc Prof Dr DYeoh

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27 Why classify? What is the implication of different CLASS?
CLASS 1 PLASTIC – able to sustain high strain and achieve plastic moment capacity and full plastic hinge in the whole cross-section; no restrictions in normal design. CLASS 2 COMPACT – achieve plastic moment capacity but with limited plastic hinge; apply plastic modulus under bending for design; elastic analysis only. CLASS 3 SEMI-COMPACT – plastic capacity not achieved; only elastic capacity; apply elastic modulus for design. CLASS 4 SLENDER – local buckling failure appear even before yield strength is achieved; apply effective section properties. Assoc Prof Dr DYeoh

28 EC3 – 6.2.4 Compression The design resistance for Class 1, 2 and 3:
Assoc Prof Dr DYeoh

29 EC3 – 6.2.5 Bending moment The design resistance for Class 1 & 2:
We will revisit this later. The design resistance for Class 4: Assoc Prof Dr DYeoh

30 How? Table 5.2 EC3 What is the type of cross-section?
What kind of stress is the section subjected to? For UB, UC or built-up sections, classify each part separately (ie. Flange and web) Calculate e factor Choose worst classification as CLASS for the section. Assoc Prof Dr DYeoh

31 Example – pure compression
Assoc Prof Dr DYeoh

32 3. Substitute ε into the class limits in Table 5.2
1. Determine fy fy = 355N/mm2 2. Determine ε 3. Substitute ε into the class limits in Table 5.2 Outstand flanges (Table 5.2, sheet 2): cf = (b – tw – 2r)/2 = mm cf / tf = / = 9ε = 7.29, 10ε = 8.10, 14ε = 11.34 Limit for Class 2 flange = 10  = > Hence flanges are Class 2 Assoc Prof Dr DYeoh

33 Web – internal compression part (Table 5.2, sheet 1):
cw = h – 2tf – 2r = mm cw / tw = 200.3/ = 33ε = 26.73, 38ε = 30.78, 42ε = 34.02 Limit for Class 1 web = 33  = > , Hence web is Class 1 4. Therefore, overall cross-section classification is Class 2. Assoc Prof Dr DYeoh

34 Cross-section compression resistance (clause 6.2.4):
Therefore, the design compression resistance of the cross-section is: Assoc Prof Dr DYeoh

35 Classification under combined bending and axial force
Classify based on the actual stress distribution of the combined loadings. STEP 1 For simplicity, classify using most severe loading condition of pure axial compression. If the section classified as Class 1 or 2, no further works are needed. STEP 2 But if the resulting section classification is Class 3 or 4, it is advisable for economy to conduct a more precise classification under the combined loading. Assoc Prof Dr DYeoh

36 Example – combined bending and axial force
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40 Comparison Separate load condition Combined load condition
Flange = CLASS 1 Web = CLASS 4 Overall = CLASS 4 Resisting capacity uses effective sectional area Flange = CLASS 1 Web = CLASS 2 Overall = CLASS 2 Resisting capacity uses whole sectional area MORE ECONOMICAL DESIGN Assoc Prof Dr DYeoh

41 End of Introduction part C
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42 Recap what have we learned?
Assoc Prof Dr DYeoh

43 Recap what have we learned?
Notations and symbols in EC3 Recap of common structural steel sections Local buckling Understanding failure modes Section classification Assoc Prof Dr DYeoh


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