Civil Engineering - Steel Structure Design - Discussion
Discussion Forum : Steel Structure Design - Section 2 (Q.No. 11)
11.
Strengths of a rivet in single shearing, in bearing and in tearing are 3425 kg, 4575 kg and 5025 kg respectively. If the load in the member is 35 tonnes, the number of rivets required, is
Discussion:
23 comments Page 2 of 3.
Ravi kumar vishwakarma said:
8 years ago
The answer should be 11 because;
n = load/rivet value.
n = 35000/3425,
n = 10.2 = 11.
n = load/rivet value.
n = 35000/3425,
n = 10.2 = 11.
Selvi said:
8 years ago
No of rivet = load/rivet vale.
Rivet value is the least value of bearing and shearing.
SO, n = 35000/3425 = 10.22 say 11.
Rivet value is the least value of bearing and shearing.
SO, n = 35000/3425 = 10.22 say 11.
Pavan said:
8 years ago
Rivets are used in WSM method. So why we multiply the load by load factor?
Then answer is 11.
Then answer is 11.
Priya said:
8 years ago
We know number of rivet = force /rivet value.
But here shearing, tearing many value given how can solve explain it.
But here shearing, tearing many value given how can solve explain it.
Dipak said:
8 years ago
11 is the right answer.
Rakesh said:
8 years ago
Bearing, shearing, and tearing strength is called Rivet value.
In bearing tearing and shearing value we take always Lower value whichever is less
Here my Rivet value is= 3428kg.
Load is = 35tonnes =35x1000=35000.
Then,
No of Rivet= load/ rivet value.
Then,
35000/3425= 10.22.
We can say 11 rivet.
In bearing tearing and shearing value we take always Lower value whichever is less
Here my Rivet value is= 3428kg.
Load is = 35tonnes =35x1000=35000.
Then,
No of Rivet= load/ rivet value.
Then,
35000/3425= 10.22.
We can say 11 rivet.
(2)
Viru kapoor said:
7 years ago
Guys it's 13.
Take fOS also.
Take fOS also.
Deep said:
7 years ago
It is 11. And no need to add FOS for matching with answer.
(1)
Amit kumar said:
7 years ago
Agree @Deep.
It should be 11.
It should be 11.
Manu said:
7 years ago
Yes, I also agree @Deep.
It is no need of FOS.
It is no need of FOS.
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