Analysis Of Truss, Method Of Joints.

In summary: Joint H is a simple 2 member truss. There is a compression force of 25 N in member H and a tension force of 35 N in member G. Since the resultant force in G must be equal and opposite to the resultant force in H, the forces are zero, and the joint is in equilibrium.Joint I is also a simple 2 member truss. There is a compression force of 25 N in member I and a tension force of 35 N in member D. Since the resultant force in D must be equal and opposite to the resultant force in I, the forces are zero, and the joint is in equilibrium.Joint J is a 3 member truss. There
  • #1
slain4ever
63
0

Homework Statement


Hi so I have the following truss:
http://screencast.com/t/BIdagRt5abg
and I need to calculate the forces in every member by method of joints

The Attempt at a Solution



So I got the Reaction forces:
F(BG) = 25N and F(AC) = 35N

Now I'm not exactually sure what to do next, I know you calculate the x and y forces at each joint, I started at C
and then I got F(y) = 0 =35N + F(CJ) sin(45)
F(CJ) = -49.497

Im fairly sure that that is right
but when I get to the horizontal my equation is like this 0=F(CJ) * Cos(45)
which doesn't seem right since it means F(CJ) is zero
can someone please help me along thx.
 
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  • #2
the equation should be 0=F(CJ) * Cos(45) + F(CD) right?

how do you tell if it is + or - ??
like is it what I wrote above or 0=F(CJ) * Cos(45) - F(CD)??
 
  • #3
After calculating reactions, you should start with the easiest joint first, a joint with only 2 members framing into it, like Joint H. This will assure you that when you get to joint C, there is no force in member CH. When you isolate joint C, look at the direction of the member forces required for equilibrium in the x and y directions. If a member force points in toward a joint, it is a compression member., and if it points away from the joint, it is a tension member. Don't forget this when you move to your next joint.

Th magnitude of your forces are thus far correct.
 
  • #4
if it is in compression does that mean its negative? or is it the other way around?

also we were told that CH, HJ, EK, GM and LM are zero force members
 
  • #5
i've calculated F(CD) to be 35 and F(DJ) = 65 F(JK) =35 and F(DK) = 91.924

i have no idea if they are negative or what
 
  • #6
i've decided to just write expressions for each of the members can you please tell me which ones I need to change to negative.

BG =25
AC = 35
CJ = -49.497
CD = 35
DJ = 65
JK = 35
DK = -91.924
DE = -(35 + -91.924* sin(45))
0 = DK sin(45) + KF sin (45) - 20
0 = JK + KL + DK sin(45) + KF sin(45)
EF = -DE
0 = GL sin(45) + BG
FG = -LG sin(45)
FL = -LG sin (45) + 10
KL = -LG sin(45)
FL = -KFsin(45)

thank you
 
  • #7
slain4ever said:
if it is in compression does that mean its negative? or is it the other way around?

also we were told that CH, HJ, EK, GM and LM are zero force members
By convention, a compression force in a member is considered a negative force, and a tension force in a member is considered a positive force. But the direction of the x and y components of these forces are determined from Newton 1, and you have to be careful about signage. This then determines whether a member is in compression or tension. If the member force (resultant of x and y components of force in that member) points toward the joint, it's a compression member...if it pulls away from the joint, it is a tension member.

slain4ever said:
i've calculated F(CD) to be 35 and F(DJ) = 65 F(JK) =35 and F(DK) = 91.924

i have no idea if they are negative or what
If you get one wrong then the others most all become wrong. Please look at Joint C first. There is a support force of 35 N acting up, and there are unknown forces CD and CJ acting along the member's long axis in an unknown direction. First realize that truss members are 2 force members...they can only take axial loads in compression or tension.

Since there is 35 N up from the support, and since no part of the vertical force can be carried by CD, then the vert comp in CJ must be 35 N down, per Newton 1. That means the horizontal comp in CJ must be 35 N to the right. The resultant force is sq rt sum of squares = 49.5 N, pulling away from the member. So CJ is in tension , call it a plus. And since since for equilibrium the force in CD must be 35 N acting left, that is a force pushing toward the joint C, so that is a compression force in CD, call it a minus.

Now move on to the other joints, tackling the joints with the least amount of unknowns first. Don't forget Newtons 3rd Law!
 

FAQ: Analysis Of Truss, Method Of Joints.

1. What is the method of joints in truss analysis?

The method of joints is a technique used in structural analysis to determine the internal forces in a truss. It involves analyzing the forces acting on each joint in a truss and using equilibrium equations to solve for the unknown forces.

2. How is the method of joints different from the method of sections?

The method of joints and the method of sections are both techniques used in truss analysis, but they differ in their approach. The method of joints focuses on analyzing each joint individually, while the method of sections cuts the truss into sections and analyzes the forces acting on the entire section.

3. What are the limitations of the method of joints?

The method of joints is limited to analyzing simple truss structures that are statically determinate, meaning that all the forces and reactions can be determined using equilibrium equations. It also assumes that all the joints are pinned and that the truss is loaded only at the joints.

4. How is the method of joints used in real-world applications?

The method of joints is commonly used in the design and analysis of truss structures, such as bridges, roofs, and cranes. It allows engineers to determine the internal forces and stresses in the truss members, ensuring that the structure can safely support the intended loads.

5. What are the steps involved in using the method of joints for truss analysis?

The first step is to analyze each joint and draw a free body diagram to determine the forces acting on it. Then, use the equilibrium equations to solve for the unknown forces. Repeat this process for each joint until all the forces in the truss are determined. Finally, check the calculations for accuracy and make any necessary adjustments.

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