BENG2 APPLIED THERMODYNAMICS
(THER 205)
TUTORIAL EXAMPLES : APPLICATIONS OF ENTROPY
1. Draw a graph of Carnot Efficiency vs
Heat input temperature (T1 ) for a heat rejection temperature
of 30ºC. (Use T1 = 100ºC
- 2000ºC). From your knowledge of material properties - what is an
approximate upper limited on hcarnot ? [soln]
2. A Carnot engine receives heat at 140 ºC
and rejects its heat via a cooling tower at 40ºC. What percentage improvement in efficiency is obtainable if it rejects its
heat to sea-water at 8ºC? [+32%]
3. Derive formulae to calculate the change
in entropy of a perfect gas when it is:
(a) heated at constant pressure from
temperature T1 to T2
.
(b) compressed at constant temperature from
p1 to p2. [soln]
Use it to
construct a T-s chart for air for pressures of 101.325 kPa and 1013.25 kPa.
(Assume
s = 0 at p1 = 101.325
kPa and T1 = 273 K)
4. A gas is throttled (suddenly reduced in
pressure) from 900 kPa to 100 kPa. No heat or work interactions occur and
velocity and height changes are negligible. What
is (a) the final temperature?
(b) the change in specific entropy?
If the gas is (A) Steam with x =
0.97, (B) Air at 28 ºC. [+0.955, +0.631
kJ/kgK]
5. A cyclic process using a perfect gas is
described by the following table:
|
Process |
Heat transfer |
Work transfer |
DU |
DS |
|
Isothermal 1®2 |
a |
2.485 kJ |
b |
c |
|
Isobaric 2®3 |
d |
e |
f |
g |
|
Adiabatic 3®1 |
h |
i |
j |
k |
|
Summations |
l |
m |
n |
p |
Calculate
the missing quantities a-p assuming each process is reversible.
(Sketch the cycle on a p-V diagram and calculate p2 , V2 , V3)
Given: V1 = 0.01 m3 , T1 =
289 K
p1 =
100 kPa, g =
1.4
6. Air expands from a pressure of 2 MPa to
30 kPa. Calculate the specific work done
if the air is at 1100 K, and the expansion is isentropic. [-776.4 kJ/kg]
7. Air is compressed in a water-cooled compressor
from 110 kPa and 15 ºC to
850 kPa and
175 ºC. Calculate the polytropic index of compression (n), and the
specific entropy change. [n=1.275, -0.142 kJ/kgK]
8. Air at 200 kPa and 425 ºC is
expanded through an adiabatic nozzle with an estimated isentropic efficiency of
0.93. If the exit pressure is 80 kPa
calculate the exit velocity. (Assume the
inlet velocity is negligible). [550 m/s]