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I'm just doing it as 2 superimposed problems. In the first part, you showed that the growth of the bar would be 14.04 mm if the bar were totally unconstrained. Since the original gap was 1 mm, that would mean that you would have to compress the bar 13.04 mm to get it to fit into the available space.ski0331 said:Where did you get the 13.04 mm? And I thought I did add them together f=-ax and f2=-ax+4000N
I'm not sure. would it? I've struggled with this subject (axial loads). But a guess would be that it would bend the brass?Chestermiller said:I'm just doing it as 2 superimposed problems. In the first part, you showed that the growth of the bar would be 14.04 mm if the bar were totally unconstrained. Since the original gap was 1 mm, that would mean that you would have to compress the bar 13.04 mm to get it to fit into the available space.
Assuming purely elastic behavior, this gives a compressive stress of 106 MPa in the Brass and a compressive stress of 131 MPa in the steel. But the yield stress of the Brass is only 78 MPa. How do you think that would affect the answer?
When you complete the solution of the purely elastic problem and have confirmed my answer, we can talk about what to do because the compressive yield stress of the brass is reached.ski0331 said:I'm not sure. would it? I've struggled with this subject (axial loads). But a guess would be that it would bend the brass?
ahhh ok I see where I did that! That makes sense, but I make my first cut to determine what Ax is for my free body diagram before the 4Kn. Like I said axial loads have been giving me fits to solve.Chestermiller said:When you complete the solution of the purely elastic problem and have confirmed my answer, we can talk about what to do because the compressive yield stress of the brass is reached.
Your solution for the elastic problem is incorrect because you included the 4000 with the steel rather than with the brass.
OK. Let's see what you get now. It seemed to me you were doing pretty well up to this point.ski0331 said:ahhh ok I see where I did that! That makes sense, but I make my first cut to determine what Ax is for my free body diagram before the 4Kn. Like I said axial loads have been giving me fits to solve.
No. You need to be careful with your arithmetic: $$-\frac{(A_x+4000)(10)}{(101\times 10^9)(100\times 10^{-6})}-\frac{(A_x)(10)}{(200\times 10^9)(50\times 10^{-6})}+0.018=0.001$$ where ##A_x## is a positive compressive force. What do you get for ##A_x##? What do you get for F from my equation in post #3?ski0331 said:
A(x) I got is equal to 6552.24, F=-6552.44Chestermiller said:No. You need to be careful with your arithmetic: $$-\frac{(A_x+4000)(10)}{(101\times 10^9)(100\times 10^{-6})}-\frac{(A_x)(10)}{(200\times 10^9)(50\times 10^{-6})}+0.018=0.001$$ where ##A_x## is a positive compressive force. What do you get for ##A_x##? What do you get for F from my equation in post #3?
I confirm. I treated F as tension and got a negative number, while you treated it as compression and got a positive number. So this is the compressive force on the steel rod, and the compressive force on the brass rod is 6552+4000=10552 N. What do these solutions to the elastic problem (neglecting the yield stress) give you for the stresses in the brass and the steel?ski0331 said:A(x) I got is equal to 6552.24, F=-6552.44
Chestermiller said:I confirm. I treated F as tension and got a negative number, while you treated it as compression and got a positive number. So this is the compressive force on the steel rod, and the compressive force on the brass rod is 6552+4000=10552 N. What do these solutions to the elastic problem (neglecting the yield stress) give you for the stresses in the brass and the steel?
ski0331 said:
ok you lost me on this chart. why are there 4p? 2 ax?Chestermiller said:
The forces on the left are the reaction forces from the constraint. The 2 P forces on the right are the applied forces. The Ax on the right is the compressive force applied on the brass section by the steel section.ski0331 said:ok you lost me on this chart. why are there 4p? 2 ax?
yes but Ax is the reaction forces of the wall. In my FBD Ax pushes back on 2p and the Normal force.Chestermiller said:The forces on the left are the reaction forces from the constraint. The 2 P forces on the right are the applied forces. The Ax on the right is the compressive force applied on the brass section by the steel section.
You are aware that tension and compression are bi-directional, arising from the application of the Cauchy stress relationship to determine the forces acting on a surface? You remember from freshman physics the tension in a rope pointing to the right (for the force the material on the right applies to the material on the left), and to the left (for the force the material on the left applies to the material on the right), correct?
Taking each section as a free body, the forces on the two ends of each section must be equal in magnitude and opposite in direction. Otherwise, the sections could not each be in force equilibrium.ski0331 said:yes but Ax is the reaction forces of the wall. In my FBD Ax pushes back on 2p and the Normal force.
Axial loading is a type of force applied to a composite beam that runs along its length, causing it to deform or bend. This can be either a compressive force, pushing the beam together, or a tensile force, pulling the beam apart.
Axial loading can significantly impact the strength of a composite beam. When the beam is under compressive loading, it may buckle or fail due to buckling. Tensile loading can cause the beam to elongate and ultimately fail due to tensile stress.
Several factors can affect how a composite beam responds to axial loading, including the material properties of the beam, the cross-sectional shape and size, the type of loading (compressive or tensile), and the boundary conditions.
The maximum axial load a composite beam can withstand is determined through various analytical and experimental methods. These include calculating the buckling load using equations, performing physical tests on the beam, and using computer simulations to model the behavior of the beam under different loading conditions.
To improve the strength of a composite beam against axial loading, various design techniques can be used. These include increasing the cross-sectional area of the beam, using materials with higher strength and stiffness, and incorporating reinforcement elements such as braces or trusses.