Respuesta :
Answer:308 K and 96.8 kJ/kg)
Explanation:
This is an isentropic process.
From the question,
Initial temperature,
T1=500∘C
p1=2MPa
Final pressure,
p2=200kPa
Checking this values from the Properties Table of Ideal Gases:
R=0.2081kJ/kg.K
Cp=0.5203kJ/kg.K
Cv=0.3122kJ/kg.K
R=0.2081 kJ/kg.KCp=0.5203 kJ/kg.KCv=
For the adiabatic value index.
γ=CpCv
=0.5203
0.3122
γ=1.67
γ=CpCv=0.52030.3122γ=1.67
(a) the outlet temperature
T2sT1=(p2p1)(γ−1γ)T2s773=(2002000)(1.67−11.67)T2s=308.K(approximately)
(b) the workdone per kg of argon during the process.
w1−2=R(T1−T2s)γ−1=0.2081(773−306.9)1.67−1w1−2=144.77kJ/kg
w1−2=R(T1−T2s)γ−1=0.2081(773−306.9)=96kj/kg
The answer to the second part of the question on work done is wrong. The right answer is 144.72 Kj/kg
Answer:
A) T2 = 308K
B) Work done per unit mass of argon = 144.72 Kj/kg
Explanation:
A) Initial temperature, T1=500∘C = 773K
Initial pressure, p1 = 2MPa = 2000KPa
Final pressure, p2=200kPa
From the ideal properties table i attached, under argo, we'll get;
R(Gas constant) = 0.2081 Kj/kg.k
Cp = 0.5203 Kj/Kg.k and Cv = 0.3122 Kj/kg.k.
Formula for adiabatic index is given as;
γ = Cp/Cv = 0.5203/0.3122 = 1.67
Now, to calculate the final temperature using temperature and pressure relationship, we have;
T2/T1 = (p2/p1)^((γ - 1)/γ)
So, T2/773 = (200/2000)^((1.67 - 1)/1.67)
T2/773 = 0.1^(0.4012)
T2/773 = 0.397
T2 = 773 x 0.397 ≈ 308K
B) Work done by turbine per unit mass of argon is given as;
W1-2 = R(T1 - T2)/(γ - 1)
W1-2 = 0.2081(773 - 306.89)/(1.67 - 1) = 96.9975/0.67 = 144.72 Kj/kg
