Molar Specific Heat: Translation Only

AI Thread Summary
In the discussion about molar specific heat, the user is trying to solve two problems related to the behavior of steam and the types of energy contributing to molar specific heat. For part (a), the user applies the adiabatic process equation but arrives at an incorrect final temperature of 147.40 K instead of the correct 235.0 K. The user is confused about the application of the equation and seeks clarification on their method. In part (b), they initially struggle with identifying the types of energy contributing to molar specific heat but later resolve that it is "translation only." The discussion highlights the importance of correctly applying thermodynamic principles to solve gas behavior problems.
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Homework Statement



(a) Steam coming from a geyser at 100°C expands as it rises into the air. Since this expansion is rapid over the first small time interval we can assume that this occurs with no heat loss to the surrounding air in the region of the vent. What happens to the temperature when its initial volume is increased to four times its initial volume?

(correct answer: 235.0 K)

(b) The ratio of Cp/Cv for a particular gas is 1.65. What are the types of energy that are contributing to the molar specific heat? Choose one of the following:

· translation only

· translation and rotation only

· translation, rotation and vibration

· translation and vibration only

(correct answer: translation only)

The Attempt at a Solution



(a) I tried this equation

T_iV_i^{\gamma-1}=T_fV_f^{\gamma-1}

100°C = 373.15 K. Also the theoretical value for \gamma is

\gamma= \frac{C_p}{C_V}=\frac{5R/2}{3R/2}= \frac{5}{3}=1.67

(373.15 K) =T_f (4^{0.67})

Tf=147.40 K

Why is my answer not correct?

(b) I don't know how to decide what types of energy are contributing to the molar specific heat. I know that the ratio of molar specefic heat is equal to 1.67 and the ratio of the particular gas given is in good adreement with this experimental values obtained for monatomic gases. But I don't know how to determine if the types of energy that are contributing to the molar specific heat are rotational/viberational/rotational. Any explanation is appreciated.
 
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Okay I figured out part (b) but I still don't know why I get part (a) wrong!

I used the equation that gives the relationship between T and V for an adiabatic process involving an ideal gas:

T_iV_i^{\gamma -1}=T_fV_f^{\gamma -1}

373.15 K = T_f 4^{0.67}

T_f=147.40

But this does not agree with the model answer (235.0 K). Is there something wrong with my method?
 
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