## List of Tension Member’s Posts-part 2.

The list of tension Member’s Posts-part 2 will start from post 7 till post 14.

- List of Tension Member's Posts-part 2.
- A Solved problem for Design strength.
- A Solved problem 4-2 for shear Lag factor U.
- Two Solved problems for the effective net area.
- Practice problem-transverse weld of a WT section.
- Practice problem-longitudinal weld of a plate section.
- Practice problem-longitudinal weld of a C-section.
- How to get an Effective area for a staggered bolted angle?

**A Solved problem for Design strength.**

This is the 7th post of the Tension Member’s Posts which includes a solved problem 3.6. from** Prof. Mccormack’s **book.

Determine the LRFD design tensile strength and the ASD allowable design tensile strength for two lines of -in diameter bolts in each flange using A572 Grade 50 steel, with the AISC Specification.

There are assumed to be at least three bolts in each line 4 in on center and the bolts are not staggered with respect to each other.

This is a link for post 7: **A Solved problem for Design strength.**

### **A Solved problem 4-2 for shear Lag factor U.**

This is the 8th post of the Tension Member’s Posts which includes a Solved problem 4.2. from Prof. Abi O. Aghayere ‘s book. The welded member is shown in fig 4.7. Determine the shear lag factor U, the net area Ant, and the effective area Ae.

This is the link to post 8: **A Solved problem 4-2 ****for shear Lag factor U.**

** Two Solved problems for the effective net area.**

This is the 9th post of the Tension Member’s Posts which includes a Solved problem 3.4 From Prof. William T Segui’s handbook. Determine the effective net area for the tension member shown in Figure 3.12.

A Solved problem 3.5, from Prof. **William T Segui’s handbook.**

If the tension member of Example 3.4 is welded as shown in Figure 3.13, determine the effective area.

This is the link to post 9: **Solved problems ****for the effective net area.**

### **Practice problem-transverse weld of a WT section.**

This is the 10th post of the Tension Member’s Posts which includes a Practice problem for the Transverse weld of a WT section., this is case 3 for the shear lag factor table D3.1. A given WT5x15 section Of A922 steel with transverse weld to its flange as shown in Figure P3-32 is required to find The LRFD and ASD values neglecting the block shear.

This is the link to post 9a: **Practice problem-transverse weld of a WT section.**

### **Practice problem-longitudinal weld of a plate section.**

This is the 11th post of the Tension Member’s Posts which includes: A given WT5x15 section Of A922 steel with transverse weld to its flange as shown in Figure P3-32 is required to find The LRFD and ASD values neglecting the block shear. The problem was solved by using CM#14. The same problem was resolved by using CM#15.

This is the link to post 9b: **Practice problem-**longitudinal weld** of a plate section.**

### Practice problem-longitudinal weld of a C-section.

This is the 12th post of the Tension Member’s Posts which includes a solved problem 3-33. from Prof. MCCormac ‘s book. This is a Practice problem for the longitudinal weld of a C section., this is case 2 for the shear lag factor table D3.1-CM-14. and also can be considered as case 4a based on CM-15 and related specification -2016.

This is the link to post 9c: Practice problem-longitudinal weld of a c-section.** **

### How to get an Effective area for a staggered bolted angle?

This is the 13th post of the Tension Member’s Posts which includes two solved problems. The first is How to get an Effective area for a staggered bolted angle. the second solved problem is how to find the service load capacity of a given bolted staggered angle. The next image is for the second solved problem.

This is the link to post 9d: How to get an Effective area for a staggered bolted angle?

This is a link to the list of tension members part 1.

This is a link to the list of tension members’ posts in part 3.

An external source for tension members from Prof. T. Bartlett Quimby’s site which is the **Tension Member Overview**