My Attempt At Re-entry Temp. Calculation

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The discussion focuses on calculating the temperature (t2) of an object using its specific heat capacity and re-entry speed. The derived equation for t2 incorporates factors like dynamic pressure and energy-temperature relationships. The accuracy of this equation in estimating temperature gain during freefall is questioned, particularly regarding the omission of skin friction effects. The approach suggests using dynamic pressure to estimate adiabatic heating, but acknowledges limitations in the model. Overall, the conversation highlights the complexities of accurately predicting temperature changes during re-entry.
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I wanted to figure out the temperature(t2) of any object based on things such as its specific heat capacity, re-entry speed, etc.

Work: W = Fy

Force by Air: FD = 1/2pv2CDA

Energy-temperature relationship: Q = mc(t2 - t1)

Setting things equal & solving for t2 gives:

t2 = (1/2pv2CDAy+mct1) / mc

(I'm sorry I could not get latex to format all of the formulas correctly so I formatted none of them...)

So, how accurate is this equation in describing temperature gain through freefall back down to earth?
 
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I'm going to take a guess and say you get an estimate by finding the dynamic pressure (q = 0.5 * density * velocity^2) and solving for the adiabatic heating due to the pressure rise. This doesn't take any skin friction into account however.
 
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