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For this problem, a = -3.6 E-13 m^3/(mol*Pa*K). The gas enters a real turbine at 547 K and 531,426 bar. If the turbine is known
For this problem, a = -3.6 E-13 m^3/(mol*Pa*K). The gas enters a real turbine at 547 K and 531,426 bar. If the turbine is known to produce -2,458.3 J/mol work, what is the temperature of its exit stream? Report your answer to one decimal place of precision and with units of K.
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