Recent content by mef51
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[Thermodynamics] Temperature change during cooling of a gas
Ohh haha the lightbulb just clicked. Perhaps the unambiguous way of phrasing it would be "Show that if both processes start at an initial pressure ##P_i## and end at a final pressure ##P_f##, then the difference in temperature obtained by the second method is always higher."- mef51
- Post #13
- Forum: Advanced Physics Homework Help
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[Thermodynamics] Temperature change during cooling of a gas
Indeed- mef51
- Post #11
- Forum: Advanced Physics Homework Help
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[Thermodynamics] Temperature change during cooling of a gas
I dunno! On a PV diagram an adiabat with constant pressure doesn't really make sense either. Let's say that we don't have this condition that the initial and final pressures are the same. Then we'd have that the temperature difference for each method is $$...- mef51
- Post #9
- Forum: Advanced Physics Homework Help
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[Thermodynamics] Temperature change during cooling of a gas
So the pressure starts and ends at the same point but changes in between?- mef51
- Post #7
- Forum: Advanced Physics Homework Help
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[Thermodynamics] Temperature change during cooling of a gas
The initial and the final pressures are the same. How do you know that? I could equivalently say that the initial temperatures are the same for both processes and the final temperatures are different. Further, it's not even necessary that any of the temperatures are the same. We just want to...- mef51
- Post #5
- Forum: Advanced Physics Homework Help
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[Thermodynamics] Temperature change during cooling of a gas
Hm okay well for adiabatic throttling I know that the Joule-Thomson coefficient ##\mu## is positive when a gas is cooling so we know that ##\mu \equiv \Big( \frac{\partial T}{\partial P} \Big)_H > 0##. Using the fact that the adiabatic throttling is a constant-enthalpy process you can show that...- mef51
- Post #3
- Forum: Advanced Physics Homework Help
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[Thermodynamics] Temperature change during cooling of a gas
Homework Statement One method for cooling a gas is adiabatic throttling (Joule-Thomson Experiment). Another method is a reversible adiabatic expansion. Show that if the initial and final pressures are the same, the difference in temperature obtained by the second method is always higher. Hint...- mef51
- Thread
- Change Cooling Gas Temperature Temperature change Thermodynamic potential Thermodynamics
- Replies: 13
- Forum: Advanced Physics Homework Help
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Graduate [Thermodynamics] Heat Capacity for Polytropic Process
It's not a homework problem. I had an attempt at it and this is what I got: (I used ##\alpha## as the polytropic index instead of ##n##) Using: ##\delta Q = nC_\alpha dT## and ##dU = nC_vdT## $$ \delta Q = dU + \delta W \\ nC_\alpha dT = nC_vdT + PdV \\ nC_\alpha \triangle T = nC_v\triangle T +...- mef51
- Post #3
- Forum: Thermodynamics
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Graduate [Thermodynamics] Heat Capacity for Polytropic Process
Consider an ideal gas. For a polytropic process we have ##PV^n = const##. Different values of ##n## will represent different processes; for example isobaric (##n=0##), isothermal (##n=1##), and isochoric (##n=\infty##). The Wikipedia article on polytropic processes states that the specific heat...- mef51
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- Capacity Heat Heat capacity Ideal gas Polytropic Process Specific heat Thermodynamics
- Replies: 3
- Forum: Thermodynamics
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[Differential Geometry] Matrix of Differential Equations in SO(3)
Okokok. Since ##Q(s)## is differentiable, it must be continuous. ##det(Q)## must also be continuous. Since ##det(Q_0) = 1##, if ##det(Q)## were ever -1, then by the Intermediate Value Theorem there should be an ##s## such that ##det(Q(s)) = 0 ## (or any other value between 1 and -1). But...- mef51
- Post #5
- Forum: Calculus and Beyond Homework Help
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[Differential Geometry] Matrix of Differential Equations in SO(3)
Since ##Q^TQ## is constant ##\forall s##, ##Q^TQ = {Q_0}^T Q_0 = I_{33}## since ##Q_0## is in ##SO(3)##. Ok. I now need to show that ##det(Q) = 1 \quad \forall s##, knowing that ##det(Q_0) = 1## I know that ##det(Q^TQ) = det(I_{33}) = 1## So using properties of determinants ##1 = det(Q^TQ) =...- mef51
- Post #4
- Forum: Calculus and Beyond Homework Help
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[Differential Geometry] Matrix of Differential Equations in SO(3)
Alright let's take the derivative of ##Q^TQ##. If this ends up being zero, then ##Q^TQ## is constant and could be equal to the identity ##I_{33}##. This would prove one of the properties we want ##Q## to have to be in ##SO(3)##. We need to use ##\dot{Q} = AQ## and ##A^T=-A## $$ (Q^TQ)' =...- mef51
- Post #3
- Forum: Calculus and Beyond Homework Help
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[Differential Geometry] Matrix of Differential Equations in SO(3)
I made a mistake in my attempt: Since ##Q_0## is constant, taking the derivative of ##Q_0## is just 0. Should perhaps take the derivative of ##A(s)Q(s)## instead- mef51
- Post #2
- Forum: Calculus and Beyond Homework Help
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[Differential Geometry] Matrix of Differential Equations in SO(3)
Homework Statement Suppose that ##s \to A(s) \subset \mathbb{M}_{33}(\mathbb{R})## is smooth and that ##A(s)## is antisymmetric for all ##s##. If ##Q_0 \in SO(3)##, show that the unique solution (which you may assume exists) to $$\dot{Q}(s) = A(s)Q(s), \quad Q(0) = Q_0$$ satisfies ##Q(s) \in...- mef51
- Thread
- Differential Differential equations Differential geometry Geometry Matrices Matrix So(3)
- Replies: 5
- Forum: Calculus and Beyond Homework Help
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[General Relativity] Prove that a tensor is a co-tensor
You're right. My prof has a convention where you only write the primes on the object instead of the indices (so ##T_{\mu\nu}'## instead of ##T_{\mu'\nu'}## and he also defined the transformation ##\Lambda## so that ##\Lambda## has a prime on the top and ##\Lambda^{-1}## has a prime on the...- mef51
- Post #5
- Forum: Advanced Physics Homework Help