Question 16.5: At the mean diameter, U = 200 m/s, V f = 180 m/s, β1 = 43.9°...
At the mean diameter, U=200 \mathrm{~m} / \mathrm{s}, V_{f}=180 \mathrm{~m} / \mathrm{s}, \beta_{1}=43.9^{\circ} and \beta_{2}=13.5^{\circ} . The factor \lambda=0.86 and \eta_{s}=0.85 and inlet temperature T_{1 t} is 288 K. Calculate the pressure ratio.
The blue check mark means that this solution has been answered and checked by an expert. This guarantees that the final answer is accurate.
Learn more on how we answer questions.
Learn more on how we answer questions.
\Delta T_{s t}=\frac{0.86 \times 200 \times 180}{1.005 \times 10^{3}}\left(\tan 43.9^{\circ}-\tan 13.5^{\circ}\right)
=22.24 \mathrm{~K}
And R_{s}=\left[1+\frac{0.85 \times 22.24}{288}\right]^{3.5}=1.25
[ c_{p} of air has been taken as 1005 J/kg K]
Related Answered Questions
Question: 16.8
Verified Answer:
(i) U_{1}=\frac{\pi \times 0.20 \times...
Question: 16.7
Verified Answer:
Specific work input w=1005 \times 30...
Question: 16.6
Verified Answer:
(i) \rho_{1}=\frac{p_{1}}{R T_{1}}=\frac{1...
Question: 16.4
Verified Answer:
Velocity of the blade tip,
U_{2}=\frac{\pi...
Question: 16.3
Verified Answer:
The absolute Mach number is the Mach number based ...
Question: 16.2
Verified Answer:
The impeller tip speed
U_{2}=\frac{\pi \ti...
Question: 16.1
Verified Answer:
(i) From Eq (16.7), we can write
T_{3 t}-T...