Design concepts

DESIGN OF CONCRETE

1. 2E4: SOLIDS & STRUCTURES Lecture 16 Dr. Bidisha Ghosh Notes: http://www.tcd.ie/civileng/Staff/Bidisha.Ghosh/Solids & Structures

2. Types of Loading There are four basic types of loading (in order of complexity). •Tension •Compression •Torsion •Bending Sometimes, two or more basic types of loading can act simultaneously on a member of a structure or machine. This is a compression testing machine. The different members are under different types of loading. 1. The specimen tested is under compression. 2. The two side bars (N) are under tension. 3. The screw is subjected to twist or torsion. 4. The crosshead is under bending.

3. Types of Loading Dead Loads : The dead load are the external loads that are relatively constant over time, including the weight of the structure itself. Live Loads: Loads that work over shorter durations, such as, weight of human beings, furniture, impact loading etc. Environmental Load (Wind Loads, Snow Loads, Earthquake Loads etc.) : When structures block the flow of wind, the wind’s kinetic energy is converted into potential energy of pressure, which causes a wind loading. Earthquakes produce loadings on structure through its interaction with the ground and its response characteristics.  Other Loads (Hydrostatic and soil pressure etc.): When structures are used to retain water, soil, or granular materials, the pressure developed by these loadings becomes an important criterion for their design.

4. How things fail? Buckling

5. How things fail? Tension

6. How things fail? Compression

7. How things fail? Bending

8. How things fail? Shear

9. How things fail? Corrosion

10. How things fail? Fatigue

11. How things fail? Torsion

12. Concepts of Design Main concept of design, Load< resistance There are mainly two types of design concepts: Allowable Stress Method This is also known as working stress method. Load and Resistance Factor Design This is also known as Limit State Design Method.

13. Allowable Stress Design (ASD) Allowable stress Structures/machines are designed for stress below yield stress or their ultimate strength to increase safety. How ? Stress due to loading <= factor of safety*yield stress

14. Working Stress Design (WSD) Each material has some ultimate strength. But it is unsafe to load a material to its ultimate strength as there can be uncertainties regarding: „ The quality of manufacture (fabrication / erection / workmanship, etc.) Load may be greater than anticipated „Material may be defective (existence of micro cracks fatigue etc .) Other unforeseen situation (calculation errors, etc.) In this case, the design stress (specifying the strength of the material) is reduced from the yield or other specified maximum to get the “allowable stress” . Based on yield stress (elastic material) (2/3 rd of yield stress) or other predetermined strain amount (for an inelastic material—e.g. for concrete, the stress at a strain of 0.3 %, allowable stress is defined. This is the earliest and most tradition design method , also least involved computationally.

15. Factor of Safety Stress due to loading <= factor of safety*yield stress Factor of safety (FS),

16. Load and Resistance Factor Design This concept is based on the ultimate strength of materials. Instead of reducing the material strength , factors are used for accounting for uncertainty in the load and the material resistance. Factors are applied to increase load and to decreases resistance, Factored load ≤ factored strength ∑ (Loads × load factors) ≤ resistance × resistance factors Load factors: e.g ., 1.4xDL + 1.7xLL ( for concrete design ) Resistance factors: 0.9xStrength of tension member More rational and complex approach. Started with concrete design, but now has been taken up by steel and more recently for designing wood. http://on.dot.wi.gov/dtid_bos/extranet/structures/LRFD/Training/LRFDvsASD_LFD-JerryD.pdf

17. Load vs. Deformation

18. FOS1

19. FOS1

20. FOS1

21. FOS1

22. FOS2

23. Types of Bolt Joint Lap joint Butt joint

24. FOS2 Double shear in 4 bolts on each side. Hence, 4*2*shear force on each bolt surface = P Shear stress should be calculated using FS. Then allowable shear stress should be multiplied with area of bolt.

25. Moment of Inertia