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
Group members:
 Muhammad Bilal Hanif ( ME151004)
 Hasnain Ahmad (ME151009)
 Muhammad Bilal Ashraf ( ME151026)
 Nadeem Iqbal ( ME151049)
 Sufian Arshad ( ME151050)
2
GROUP # 04
Steady Flow Energy
Equation
Presentation of
Thermodynamics-I
Topic on
Assigned by:
Dr. Ijaz Khan
What is SFEE?
A steady flow process is one in
which matter and energy flow
steadily.
ṁin = ṁout
Unsteady flow is:
ṁin ≠ ṁout
Derivation of Steady Flow Equation
By the conservation of energy states:
Energy(in) = Energy(out)
  )
2
()
2
( 1
2
1
112
2
2
22 gzhmgzhmWQ
VV

0)
2
()
2
( 2
2
2
221
2
1
11   gzhmgzhmWQ
VV

mmm   12since
)
2
()
2
( 1
2
1
12
2
2
2 gzhmgzhmWQ 
VV

Then;
)](
2
[ 12
2
1
2
2
12 zzghhmWQ 


VV

)(
2
12
2
1
2
2
12 zzghhWQ 


VV
Dividing the equation by m yields
Uniform-Flow Processes
At any instant during the process,
the state of control volume is
uniform
The fluid properties may differ
from one inlet or exit to another,
 But the fluid flow at an inlet or
exit is uniform and steady
Applications of SFEE:
Nozzles and Diffusers:
 Nozzles and diffusers are properly shaped
ducts
 used to increase or decrease the speed of the
fluid
q = Δh + ΔV2 / 2 + gΔz + w
q = 0 Δz = 0 w = 0
21
2
2
1
then hh V
)(2 21 hh V
Steam Turbine:
from q = Δh + ΔV2 / 2 + gΔz + ws
if q = 0; Δc = 0; Δz = 0
then ws = -Δh
= h1 - h2
 A turbine is a device
 With rows of blades mounted on a shaft
 Could be rotated about its axis
Throttling Valves:
From q = Δh + ΔV2 / 2 + gΔz + ws
as q = 0; ws = 0; z = 0 ; ΔV2 / 2 =0
then Δh =0
That is h1 = h2
A throttling valve is a device
Used to cause a pressure drop in a flowing
fluid.
It does not involve any work.
Heat exchangers:
From q = Δh + ΔV2 / 2 + gΔz + ws
as q = 0; ws = 0; Δ z = 0;ΔV2 / 2 =0
Δh =0
That is ∑hin = ∑ hexit
It is a device
Hot fluid stream exchanges heat
with a cold fluid stream
Without mixing with each other
SFEE for More Than One Outlet:
Energy(in) = Energy(out)
See
Blow
Pic
.
.
.
.
.
)(
2
213
2
2
1
2
3
213 zzzg
V
hhhWQ 


VV
1
2
3
1
2
3
  )(
2
)(
2
3
2
3
321
2
2
2
1
21 zghWzzg
VV
hhQ 




 

V
Non-Flow Energy Equation:-
When the fluid in closed system
It is not passing through the
system boundary
The flow terms in SFEE will not
apply
In derivation of it u neglect PV
and
 velocity
Equation of non-Flow Equation:-
U1 + Q = U2 + W
Q = (U2 –U1) + W
Q = ∆U + W
Hence,
Heat Transferred the boundary of system
= change of internal energy + work done
Problem # 01 :-
Steam enter a turbaine with velocity of 16m/sec and sp. enthalpy 2990kj/kg.
The steam leaves the turbine with velocity of 37m/s and sp. enthalpy
2530kJ/kg . The heat lost to the surrounding as the steam passes through the
turbine is 25kJ/kg. The steam flow rate is 324000kg/hour. Determine the work
out in kw (power).
Given;
ṁ = 32400kg/hr
P = w/m x ṁ
By equation of SFFEE , we will find w/m
and in above equation we get power
Bernoullie’s Equation:
 By the help SFEE we can derive Bernoullie’s
equation
 If there is no change in internal energy
 Q = 0 ,
 W = 0
Then Equation will remain of Bernoullie’s Eq.
Problem# 02
 Steam flows along a horizontal duct . At one point in the duct
the pressure of steam is 1 bar and the temperature is 400℃. At
a second point some distance from first , the pressure is 1.5 bar
and temp. is 500℃. Assuming flow is be friction less and
adiabatic . Determine whether the flow is accelerating or
decelerating.
 Solve:
 In SFEE we put the values like w = 0, Q
= 0, PE = 0
 Then we will get ;
 h2-h1 = -∆𝑉2
2
 So flow is decelerating as we negative value.
Problem # 03
 Steam is expanded isentropically in a turbine
from 30 bar 400℃ 𝑡𝑜 4 𝑏𝑎𝑟. Calculate the
work done per unit mass flow of steam.
Neglect changes as K.E and P.E.
 Solve:
 Q = 0, K.E = P.E = 0,
 Hence ;
 W = m [h2-h1]
 By table , we get h1 = 3230.9kJ/kg, h2 =
2750kJ/kg & m = 1
 Hence we get;
 Answer by putting values in above Eq.
Problem# 04
 A compressor takes in air at 1 bar and 20℃.and discharge into line. The average
air velocity in the line at appoint close the discharge is 0.7m/s and discharge
pressure is 3.5 bar. Assuming isentropically, calculate the work input to
compressor .Assume that air inlet velocity is very small.
 Slove:
 By putting the value Q=0 & P.E=0 in SFEE Eq. we get this relation:
-W=𝑚{∆ℎ +
∆𝑉2
2
} then
 -W=𝑚{𝐶𝑝. ∆𝑇 +
∆𝑉2
2
}
 T1 and P1 and P2 is given by this we get T2:
 T2=T1(
𝑃2
𝑃1
)
𝑛−1
𝑛
 So put this values in above Eq. and Required
Answer.
Problem #05
 Air is expanded isentropically in a nozzle from 13.8 bar and 150℃. To
a presume of 6.9 bar. The inlet velocity to the nozzle is very small
and process occur under steady flow. Calculate the exit velocity from
the nozzle knowing that the nozzle is laid in a horizontal plane and
that the inlet is 10m/s.
Solve:
 By putting these Q = 0 , P.E = 0, w = 0 .So SFEE is:
 0= m[Cp(T2-T1)+
∆𝑉2
2
]
 By the calculating T2 from
T2=T1(
𝑃2
𝑃1
)
𝑛−1
𝑛
 Then putting values in above Eq.
 Get Answer
THANKS for
Bearing Us.
From our side it is
enough.

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Steady flow energy eq....by Bilal Ashraf

  • 1.
  • 2.  Group members:  Muhammad Bilal Hanif ( ME151004)  Hasnain Ahmad (ME151009)  Muhammad Bilal Ashraf ( ME151026)  Nadeem Iqbal ( ME151049)  Sufian Arshad ( ME151050) 2 GROUP # 04
  • 3. Steady Flow Energy Equation Presentation of Thermodynamics-I Topic on Assigned by: Dr. Ijaz Khan
  • 4. What is SFEE? A steady flow process is one in which matter and energy flow steadily. ṁin = ṁout Unsteady flow is: ṁin ≠ ṁout
  • 5. Derivation of Steady Flow Equation By the conservation of energy states: Energy(in) = Energy(out)   ) 2 () 2 ( 1 2 1 112 2 2 22 gzhmgzhmWQ VV  0) 2 () 2 ( 2 2 2 221 2 1 11   gzhmgzhmWQ VV 
  • 6. mmm   12since ) 2 () 2 ( 1 2 1 12 2 2 2 gzhmgzhmWQ  VV  Then; )]( 2 [ 12 2 1 2 2 12 zzghhmWQ    VV  )( 2 12 2 1 2 2 12 zzghhWQ    VV Dividing the equation by m yields
  • 7. Uniform-Flow Processes At any instant during the process, the state of control volume is uniform The fluid properties may differ from one inlet or exit to another,  But the fluid flow at an inlet or exit is uniform and steady
  • 8. Applications of SFEE: Nozzles and Diffusers:  Nozzles and diffusers are properly shaped ducts  used to increase or decrease the speed of the fluid q = Δh + ΔV2 / 2 + gΔz + w q = 0 Δz = 0 w = 0 21 2 2 1 then hh V )(2 21 hh V
  • 9. Steam Turbine: from q = Δh + ΔV2 / 2 + gΔz + ws if q = 0; Δc = 0; Δz = 0 then ws = -Δh = h1 - h2  A turbine is a device  With rows of blades mounted on a shaft  Could be rotated about its axis
  • 10. Throttling Valves: From q = Δh + ΔV2 / 2 + gΔz + ws as q = 0; ws = 0; z = 0 ; ΔV2 / 2 =0 then Δh =0 That is h1 = h2 A throttling valve is a device Used to cause a pressure drop in a flowing fluid. It does not involve any work.
  • 11. Heat exchangers: From q = Δh + ΔV2 / 2 + gΔz + ws as q = 0; ws = 0; Δ z = 0;ΔV2 / 2 =0 Δh =0 That is ∑hin = ∑ hexit It is a device Hot fluid stream exchanges heat with a cold fluid stream Without mixing with each other
  • 12. SFEE for More Than One Outlet: Energy(in) = Energy(out) See Blow Pic . . . . . )( 2 213 2 2 1 2 3 213 zzzg V hhhWQ    VV 1 2 3 1 2 3   )( 2 )( 2 3 2 3 321 2 2 2 1 21 zghWzzg VV hhQ         V
  • 13. Non-Flow Energy Equation:- When the fluid in closed system It is not passing through the system boundary The flow terms in SFEE will not apply In derivation of it u neglect PV and  velocity
  • 14. Equation of non-Flow Equation:- U1 + Q = U2 + W Q = (U2 –U1) + W Q = ∆U + W Hence, Heat Transferred the boundary of system = change of internal energy + work done
  • 15. Problem # 01 :- Steam enter a turbaine with velocity of 16m/sec and sp. enthalpy 2990kj/kg. The steam leaves the turbine with velocity of 37m/s and sp. enthalpy 2530kJ/kg . The heat lost to the surrounding as the steam passes through the turbine is 25kJ/kg. The steam flow rate is 324000kg/hour. Determine the work out in kw (power). Given; ṁ = 32400kg/hr P = w/m x ṁ By equation of SFFEE , we will find w/m and in above equation we get power
  • 16. Bernoullie’s Equation:  By the help SFEE we can derive Bernoullie’s equation  If there is no change in internal energy  Q = 0 ,  W = 0 Then Equation will remain of Bernoullie’s Eq.
  • 17. Problem# 02  Steam flows along a horizontal duct . At one point in the duct the pressure of steam is 1 bar and the temperature is 400℃. At a second point some distance from first , the pressure is 1.5 bar and temp. is 500℃. Assuming flow is be friction less and adiabatic . Determine whether the flow is accelerating or decelerating.  Solve:  In SFEE we put the values like w = 0, Q = 0, PE = 0  Then we will get ;  h2-h1 = -∆𝑉2 2  So flow is decelerating as we negative value.
  • 18. Problem # 03  Steam is expanded isentropically in a turbine from 30 bar 400℃ 𝑡𝑜 4 𝑏𝑎𝑟. Calculate the work done per unit mass flow of steam. Neglect changes as K.E and P.E.  Solve:  Q = 0, K.E = P.E = 0,  Hence ;  W = m [h2-h1]  By table , we get h1 = 3230.9kJ/kg, h2 = 2750kJ/kg & m = 1  Hence we get;  Answer by putting values in above Eq.
  • 19. Problem# 04  A compressor takes in air at 1 bar and 20℃.and discharge into line. The average air velocity in the line at appoint close the discharge is 0.7m/s and discharge pressure is 3.5 bar. Assuming isentropically, calculate the work input to compressor .Assume that air inlet velocity is very small.  Slove:  By putting the value Q=0 & P.E=0 in SFEE Eq. we get this relation: -W=𝑚{∆ℎ + ∆𝑉2 2 } then  -W=𝑚{𝐶𝑝. ∆𝑇 + ∆𝑉2 2 }  T1 and P1 and P2 is given by this we get T2:  T2=T1( 𝑃2 𝑃1 ) 𝑛−1 𝑛  So put this values in above Eq. and Required Answer.
  • 20. Problem #05  Air is expanded isentropically in a nozzle from 13.8 bar and 150℃. To a presume of 6.9 bar. The inlet velocity to the nozzle is very small and process occur under steady flow. Calculate the exit velocity from the nozzle knowing that the nozzle is laid in a horizontal plane and that the inlet is 10m/s. Solve:  By putting these Q = 0 , P.E = 0, w = 0 .So SFEE is:  0= m[Cp(T2-T1)+ ∆𝑉2 2 ]  By the calculating T2 from T2=T1( 𝑃2 𝑃1 ) 𝑛−1 𝑛  Then putting values in above Eq.  Get Answer
  • 21. THANKS for Bearing Us. From our side it is enough.