- The Point Loads Are Placed At The Foxed Positions Shown In The Figure And They Are Five Loads C Centre F C 38mpafc 1 (48.47 KiB) Viewed 30 times
- The Point Loads Are Placed At The Foxed Positions Shown In The Figure And They Are Five Loads C Centre F C 38mpafc 2 (66.98 KiB) Viewed 30 times
- The Point Loads Are Placed At The Foxed Positions Shown In The Figure And They Are Five Loads C Centre F C 38mpafc 3 (95.25 KiB) Viewed 30 times
- The Point Loads Are Placed At The Foxed Positions Shown In The Figure And They Are Five Loads C Centre F C 38mpafc 4 (77.99 KiB) Viewed 30 times
I need help with the entire question with detailed if possibleit will be helpful for my study,thank you
The point loads are placed at the foxed positions shown in the figure and they are five loads. C (centre) f′c′=38Mpafct,f′=3.5MPafsy=500MPaEs=200GPaEc=28600MPa Variables
P=2kN are applied at the positions shown in the figure. (Note: The load factor for G is 12 and for P is 1.5. There is no uniformly distributed five load.) 1.1 Find the maximum moment of the beam. Mr. kNm(1 mark) 1.2 Find the neutral axis distance from the top surface. If the section is governed by the linear elastic regime the transformed area method dn=∑yiA4/∑Ai is valid. mm (1 mark) 1.3 Find the cracking moment. Me= Nm(2 mark) 1.4 Does this section crack? (1 mark) valid. However. we may need to solve the quadratic equation for calculating the neutral axis distance from the top surface.
valid. However, we may need to solve the quadratic equation for calculating the neutral axis distance from the top surface.
mm(2 marks) kNm (2 marks) concrete section and independent to the applied loads. positions shown in the figure. Determine if the design moment strength (φM i ) exceeds the factored design moment M". φ in 0.85.