Please let me know if I did anything wrong on this thermo problem

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The discussion centers on solving a thermodynamics problem involving an adiabatic and rigid open vessel containing air. The user correctly applies the foundational energy balance equation, leading to the expression for the instantaneous rate of extensive energy increase as dE/dt = (dot{m} * k * R * T_{in}) / (k - 1). Key parameters include the incoming air temperature of 450 K, a mass flow rate of 0.10 kg/s, and a specific heat ratio (k) of 1.40. The consensus confirms that additional variables such as pressure and control volume mass are unnecessary for this calculation.

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RagincajunLA
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I have a homework problem that I completed but I am not sure if it is correct. I was wondering if you guys could let me know if my thought process is correct of if I need to modify my solution. The problem is:

An adiabatic and rigid open vessel contains 4 kg of air at 300 K and has a volume of 1m^3. Air at 450 K and 400 kPa is entering the vessel at a rate of 0.10 kg/s. Assume the air is calorimetrically perfect ideal gas (CPIG) with constant specific heat ratio (k) of 1.40. What is the instantaneous rate of extensive energy increase in the vessel?

I started off by completing a foundational energy balance of

\frac{dE}{dt}=\frac{dU}{dt}+\frac{dKE}{dt}+\frac{dPE}{dt}=\frac{dU}{dt}=\dot{m}_{in}T_{in}

Since this is a CPIG, its enthalpy can be simplified to h_{in}in=c_{p}T_{in} and the constant pressure specific heat can be simplified to c_{p}=\frac{kR}{k-1}. By using all this, I get a final expression of

\frac{dE}{dt}=\frac{dU}{dt}=\frac{\dot{m}kRT_{in}}{k-1}

where Tin is the temperature of the incoming air.

For some reason I felt like I left some stuff out of the problem. For instance, I wasn't sure if I needed to use the pressure of the incoming air, the mass of the air in the control volume, or the volume of the control volume. Please let me know If I completed this problem correctly or steer me in the right direction. Thank you
 
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.Yes, you have completed the problem correctly. You do not need to use the pressure of the incoming air, the mass of the air in the control volume, or the volume of the control volume. The only variables you need to use are the rate of mass flow of the incoming air, the constant specific heat ratio, and the temperature of the incoming air.
 

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