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Propeller Cavitation
The Phenomenon of Cavitation
Cavitation is a general fluid
mechanics phenomenon which
can occur whenever a liquid
used in a machine which
induces pressure and velocity
fluctuations in the fluid (e.g.
Pumps, turbines, propellers,
bearings,..)
When cavitation occurs the
liquid changes its phase into
vapor at certain flow region
where local pressure is very low
due to the high local velocities
There are two types of vaporization:
Vaporization by increasing temperature
(boiling)
Vaporization under nearly constant
temperature due to reduced pressure
(i.e. cold boiling)
The cold boiling process and hence
cavitation depends on the purity of
water.
If water contains a significant amount of
dissolved air, hence as the pressure
decreases the air comes out of the
solution and forms cavities in which the
pressure will be greater then the “vapor
pressure”.
This small tunnel is still
kept in working order at
the Marine Technology
Dept. of Newcastle Univ.
Parsons also constructed
a larger tunnel 15 years
later in which he could
test 12” diameter
propeller model
Cavitation Number
Types of Cavitation
Hub Vortex Cavitation
Face Cavitation
Effects of Cavitation on Propellers
• Cavitation phenomenon can happen any part of a ship hull where the
local pressures are very low.
• The propeller itself is the greater source of cavitation.
• When cavitation occurs depending upon its extend and severity, the
propeller may suffer from
• Performance breakdown
• Noise , Vibration , Erosion
Examples of Full Scale Cavitation
Cavitation Reporting
Cavitation Calculation
T.E.
L.E.
SUCTION SIDE
T.E.
L.E.
PRESSURE SIDE
r/R=0.2300
r/R=0.3000
r/R=0.4000
r/R=0.5000
r/R=0.6000
r/R=0.7000
r/R=0.8000
r/R=0.8500
r/R=0.9000
r/R=0.9500
r/R=0.9750
r/R=1.0000
CAVITATION ANALYSIS
FOR 0.0 DEGREES FROM UPWARD
TIP VORTEX SHED FROM SUCTION SIDE
SHEET CAVITATION ON SUCTION SIDE (11.9 %)
NO BUBBLE CAVITATION DETECTED
V1
V2
-1 -0.5 0 0.5 1 1.5 2 2.5 3
-0.5
0
0.5
1
1.5
2
2.5
3
3.5
0.0
1
0
.0
2
0
.
0
3
0
.
0
4
0
.
0
50.0
60.0
70.0
80.0
90.0
100.0
110.0
120.0
130.0
1
4
0
.
0
1
5
0
.
0
1
6
0
.
0
1
7
0
.0
180.0
1
9
0
.0
2
0
0
.
0
2
1
0
.
0
2
2
0
.
0
230.0
240.0
250.0
260.0
270.0
280.0
290.0
300.0
310.0
3
2
0
.
0
3
3
0
.
0
3
4
0
.
0
3
5
0
.0
r/R-x
r/R-y
-1.5 -1 -0.5 0 0.5 1 1.5
-1.5
-1
-0.5
0
0.5
1
1.5
Vx/Vs
0.95
0.90
0.85
0.80
0.75
0.70
0.65
0.60
0.55
Preventation of Cavitation
Preventation of Cavitation
Cavitation Criteria
T/Ap=77.57 kPa (11.25 lbf/in2)
Tip Speed=61 m/s (=πnD)
Burrill and Keller Criteron
0.7R

C

Permissible level of back
cavitation
0
; Thrust LoadingCoefficient
Thrust
PropellerProjectedArea
Staticalpressureatshaftcenterline
saturatedvaporpressure( . . )
dynamicalpressurecalculatedat 0.7
P
c
T
P
V
T
T
A
q
T
A
P
e i e P
q r R
 




 
2
1
2
T R
q V


0
;
P
c R
T T
T
P e
A
q q
 

 
   
2 2
2
2
2 2
2
2
in knots
1
in RPM
2 7.12 3.29
infeet
or
in knots
1
11.66 0.828 in RPM
2
in meters
a
a
T R
a
T R a
V
V ND lbs
q V N
in
D
V
N
q V V ND N
m
D




     
   
     
      



 
   
 
  



L
2
2
totalstaticheadatshaftC - VaporPressure
( )
(14.45 0.45 infeet
or
99629 10179 in meters
a
p e
P gH e
lbs
H H
in
N
p e H H
m

 
  
 
   
 
 
    
 
0
2
2
0
2
2
in HP
2.26
in knots
infeet
or
in kW
1941.3
in knots
in meters
D
D
a
P a P
P
D
D
a
P a P
P
P
T P lbs
V
A V A in
A
P
T P N
V
A V A m
A




 
 
 
  



 
 
 
  

• In using Burrill’s diagram from the value of τc read off from
the diagram the projected area for the propeller can be
calculated from the following;
• To derive the expanded area from the projected area, Burrill
provides the emprical realtionship which is valid for
conventional propeller forms only;
• Expanded blade area ratio - EAR
P
c T
T
A
q


 
( )
1.067 0.229
P
E E D
A
A A A assumed
P
D
 

2
0
4
E E
A A
D
A 

KELLER’s Criteria
• The alternative blade area estimation is the Keller Formula
• Where
• P0 is the static pressure at the shaft Center Line in Pa
• PV is the vapor pressure in Pa (~1700 N/m2)
• T is the propeller thrust (N)
• Z is the blade number
• D is the propeller diameter in meters
 
  2
0 0
1.3 0.3
E
V
Z T
A
K
A P P D

 

0.2for single screws
0.0for fast naval ships
Twin Screws
0.1for slow merhantships
K
K
K

 

 
Propeller_Cavitation.pptx
Propeller_Cavitation.pptx

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Propeller_Cavitation.pptx

  • 2. Cavitation is a general fluid mechanics phenomenon which can occur whenever a liquid used in a machine which induces pressure and velocity fluctuations in the fluid (e.g. Pumps, turbines, propellers, bearings,..) When cavitation occurs the liquid changes its phase into vapor at certain flow region where local pressure is very low due to the high local velocities There are two types of vaporization: Vaporization by increasing temperature (boiling) Vaporization under nearly constant temperature due to reduced pressure (i.e. cold boiling) The cold boiling process and hence cavitation depends on the purity of water. If water contains a significant amount of dissolved air, hence as the pressure decreases the air comes out of the solution and forms cavities in which the pressure will be greater then the “vapor pressure”.
  • 3. This small tunnel is still kept in working order at the Marine Technology Dept. of Newcastle Univ. Parsons also constructed a larger tunnel 15 years later in which he could test 12” diameter propeller model
  • 4.
  • 5.
  • 7.
  • 9.
  • 10.
  • 11.
  • 13.
  • 15.
  • 16.
  • 17. Effects of Cavitation on Propellers • Cavitation phenomenon can happen any part of a ship hull where the local pressures are very low. • The propeller itself is the greater source of cavitation. • When cavitation occurs depending upon its extend and severity, the propeller may suffer from • Performance breakdown • Noise , Vibration , Erosion
  • 18.
  • 19.
  • 20.
  • 21. Examples of Full Scale Cavitation
  • 23. Cavitation Calculation T.E. L.E. SUCTION SIDE T.E. L.E. PRESSURE SIDE r/R=0.2300 r/R=0.3000 r/R=0.4000 r/R=0.5000 r/R=0.6000 r/R=0.7000 r/R=0.8000 r/R=0.8500 r/R=0.9000 r/R=0.9500 r/R=0.9750 r/R=1.0000 CAVITATION ANALYSIS FOR 0.0 DEGREES FROM UPWARD TIP VORTEX SHED FROM SUCTION SIDE SHEET CAVITATION ON SUCTION SIDE (11.9 %) NO BUBBLE CAVITATION DETECTED V1 V2 -1 -0.5 0 0.5 1 1.5 2 2.5 3 -0.5 0 0.5 1 1.5 2 2.5 3 3.5 0.0 1 0 .0 2 0 . 0 3 0 . 0 4 0 . 0 50.0 60.0 70.0 80.0 90.0 100.0 110.0 120.0 130.0 1 4 0 . 0 1 5 0 . 0 1 6 0 . 0 1 7 0 .0 180.0 1 9 0 .0 2 0 0 . 0 2 1 0 . 0 2 2 0 . 0 230.0 240.0 250.0 260.0 270.0 280.0 290.0 300.0 310.0 3 2 0 . 0 3 3 0 . 0 3 4 0 . 0 3 5 0 .0 r/R-x r/R-y -1.5 -1 -0.5 0 0.5 1 1.5 -1.5 -1 -0.5 0 0.5 1 1.5 Vx/Vs 0.95 0.90 0.85 0.80 0.75 0.70 0.65 0.60 0.55
  • 26.
  • 27. Cavitation Criteria T/Ap=77.57 kPa (11.25 lbf/in2) Tip Speed=61 m/s (=πnD)
  • 28. Burrill and Keller Criteron
  • 30.
  • 31.
  • 32. 0 ; Thrust LoadingCoefficient Thrust PropellerProjectedArea Staticalpressureatshaftcenterline saturatedvaporpressure( . . ) dynamicalpressurecalculatedat 0.7 P c T P V T T A q T A P e i e P q r R         2 1 2 T R q V   0 ; P c R T T T P e A q q          2 2 2 2 2 2 2 2 in knots 1 in RPM 2 7.12 3.29 infeet or in knots 1 11.66 0.828 in RPM 2 in meters a a T R a T R a V V ND lbs q V N in D V N q V V ND N m D                                          
  • 33.   L 2 2 totalstaticheadatshaftC - VaporPressure ( ) (14.45 0.45 infeet or 99629 10179 in meters a p e P gH e lbs H H in N p e H H m                        0 2 2 0 2 2 in HP 2.26 in knots infeet or in kW 1941.3 in knots in meters D D a P a P P D D a P a P P P T P lbs V A V A in A P T P N V A V A m A                          
  • 34. • In using Burrill’s diagram from the value of τc read off from the diagram the projected area for the propeller can be calculated from the following; • To derive the expanded area from the projected area, Burrill provides the emprical realtionship which is valid for conventional propeller forms only; • Expanded blade area ratio - EAR P c T T A q     ( ) 1.067 0.229 P E E D A A A A assumed P D    2 0 4 E E A A D A  
  • 35. KELLER’s Criteria • The alternative blade area estimation is the Keller Formula • Where • P0 is the static pressure at the shaft Center Line in Pa • PV is the vapor pressure in Pa (~1700 N/m2) • T is the propeller thrust (N) • Z is the blade number • D is the propeller diameter in meters     2 0 0 1.3 0.3 E V Z T A K A P P D     0.2for single screws 0.0for fast naval ships Twin Screws 0.1for slow merhantships K K K      