Question: 3 . 1 . 1 . 1 CONVERTING DISTRIBUTED LOADS TO POINT LOADS Unfortunately, both our live and dead loads are distributed loads. We have

3.1.1.1 CONVERTING DISTRIBUTED LOADS TO POINT LOADS
Unfortunately, both our live and dead loads are distributed loads. We have to convert the distributed loads into point loads at the joints.
To see how to do this, let's looks at the live load acting on member AB . The live load acting on AB is qL2(force q per unit length time length L2). Because the live load is uniformly distributed along AB , we see that half of it can be allocated to joint A and half to joint B, or qL4 at A and qL4 at B .
Now lets look at the live load acting on member BC. Again, the total force is qL2. Half is allocated to each end of BC, or qL/4 at B and qL4 at C .
The total live load acting on joint A is qL4. The total live load acting on joint B is qL2(qL4 from member AB and qL4 from member BC ). The total live load acting on joint C is qL4
LLA=q*L4
LLB=q*L2
LLC=q*L4
LLD=0
LLE=0
We can perform a similar analysis to find the dead load acting at each point. Half the weight of member AB is allocated to joint A, half to Joint B. So on and so forth.
DLA=wAB+wAE2
DLB=wAB+wBC+wBD+wBE2
DLC=wBC+wCD2
DLD=wBD+wCD+wDE2
DLE=wAE+wBE+wDE2
3.1.2 Overall Equilibrium Equations
Now that the free body diagram is complete, we do our equilibrium equations. This is a 2D rigid body problem, so there are three degrees of freedom and three equilibrium equations. There are no forces in x , and symmetry tells us that RAy and RBy must be equal.
RAy=RCy=DL+LL2
3.1.3 Jont Level FBDs and Equilibrium Equations3.1.1.1 CONVERTING DISTRIBUTED LOADS TO POINT LOADS
Unfortunately, both our live and dead loads are distributed loads. We have to convert the distributed loads into point loads at the joints.
To see how to do this, let's looks at the live load acting on member AB . The live load acting on AB is qL2(force q per unit length time length L2). Because the live load is uniformly distributed along AB , we see that half of it can be allocated to joint A and half to joint B, or qL4 at A and qL4 at B .
Now lets look at the live load acting on member BC. Again, the total force is qL2. Half is allocated to each end of BC, or qL/4 at B and qL4 at C .
The total live load acting on joint A is qL4. The total live load acting on joint B is qL2(qL4 from member AB and qL4 from member BC ). The total live load acting on joint C is qL4
LLA=q*L4
LLB=q*L2
LLC=q*L4
LLD=0
LLE=0
We can perform a similar analysis to find the dead load acting at each point. Half the weight of member AB is allocated to joint A, half to Joint B. So on and so forth.
DLA=wAB+wAE2
DLB=wAB+wBC+wBD+wBE2
DLC=wBC+wCD2
DLD=wBD+wCD+wDE2
DLE=wAE+wBE+wDE2
3.1.2 Overall Equilibrium Equations
Now that the free body diagram is complete, we do our equilibrium equations. This is a 2D rigid body problem, so there are three degrees of freedom and three equilibrium equations. There are no forces in x , and symmetry tells us that RAy and RBy must be equal.
RAy=RCy=DL+LL2
3.1.3 Jont Level FBDs and Equilibrium Equations
3 . 1 . 1 . 1 CONVERTING DISTRIBUTED LOADS TO

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