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CAV2012, August 14-16, 2012, Singapore. Influence of ventilation on the shape of slender axisymmetric cavities. Igor Nesteruk Institute of Hydromechanics National Academy of Sciences of Ukraine. [email protected]. The steady flow pattern and the following assumptions are used:. - PowerPoint PPT Presentation
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Influence of ventilationon the shape of slender axisymmetric cavities
Igor Nesteruk
Institute of Hydromechanics National Academy of Sciences of Ukraine
CAV2012, August 14-16, 2012, Singapore
The steady flow pattern and the following assumptions are used:
1. External water flow is axisymmetric potential, inviscid and incompressible
2. Internal gas flow is one dimensional, inviscid and incompressible
3. Gravity and capillarity forces are neglected4. Cavitator, cavity and hull are slender
1/ cm LR
The external water flow potential and Bernoulli equation (Cole, 1968)
)ln()(ln)(
)(ln),,(24
*2
2
OxBrxA
xAxrx
1
0
ln)()(
2
1
dxxsignd
dA 2ln)()( xAxB
r
r*dx
dFF)x(A ,
)x(R
)x(F,
)(ln1)( 22
2222
)( O
dx
Rd
dr
d
dx
dxC
xRrp
Bernoulli and continuity equations for the internal gas flow
2
)(
2)(
220
0
xVVpxp gg
QxRxRxVRRV bb )()()()( 2220
200
222220
20
22
2
0 )(
1
)(
1)(
bb
gp RRRRU
Qxc
Basic differential equation and initial conditions (Manova, Nesteruk&Shepetyuk 2011)
])(
1[
ln 2220
2
22
bRRa
dx
Rd
ln240
2
2
UR
Qg 220
20 ]1[
R
Ra b
20
0
)(2
U
pp
At the cavity surface:
(1)
; ;
Initial conditions at : ;
flowgasinpwaterinp xCxC )()(
0x 1R dxdR /
Cavities on cylindrical hulls ;)( 0 constRxR bb
;0 Veeff
:)1(. Eq
)/()(ln 22 UUaVe gg
Base ventilated cavity on a cylindrical hull
;/2 dxdRu
)2()1(
1
)(
1
ln
)1(
2
420
20
2
222
bb
eff
RRR
Ru
Cavities on cylindrical hulls, (Manova, Nesteruk&Shepetyuk 2011)
0
;1.00
;1.0 0bb RR
Semi-length and maximum radius of ventilated cavities at:
= 0; 0.5; 0.8; 0.9; 0.99 (curves 1-5 respectively)
Cavities on cylindrical hulls,Critical values of ventilation rate, corresponding to unlimited cavities
0
;1.00 ;1.00bb RR = 0; 0.5; 0.8; 0.9 (curves 1-4)
0)1(
1
)(
1
ln
)1(2
2
0
2
0
2
2
2
bbm
meff
RRR
R
:)2(. Eq
ln/01 acr
01 crVe
:)1/()ln2( 20
200 bcr Rfor
.)(2 Figinlinessolidexistscr
Base cavities on cylindrical hulls, Ventilation diminishes the length (Nesteruk&Shepetyuk
2011)
;00 ;1.0 0bb RR Base cavity length at:= 0; 0.5; 0.8; 0.9(curv.1-
4)
0
0 1.0
1.0 1.0
Asymptotic solution at small values of the ventilation rate
)()()()( 22)2(
2)1(
2 OxRxRxR
12ln2
)(2
2)1( x
xxR eff
2
02
12
12
)1(
1
0
22
)2()()(
)(x
b
x
xRxR
dxdxxR
1.00
;1.0
))1(.,51(
99.0;9.0;8.0;5.0;00
eqcurves
RR bb
)(: )1( xRlinedashed
Cavities on conical-cylindrical hulls.Calculations at the fixed conical part length and different values of cylinder radius (Nesteruk&Shepetyuk 2012)
171 x
1R
6.11 R 7.11 R
21 R
2.21 R
CONCLUSIONS
Ventilated steady slender axysimmetric cavity is considered with the use of one-dimensional inviscid flow of the incompressible gas in the channel between the cavity surface and the body of revolution. The non-linear differential equation and its numerical and asymptotic solutions were obtained.
For the disc and cone cavitators the ventilation can sufficiently
increase the cavity dimensions and its rate is limited by two critical values. Ventilation sufficiently decreases the base cavity length.
Examples of calculations for cylindrical and cone-cylindrical shapes of the body located in the cavity are presented. It was shown that the cavity shape depends sufficiently on the values of Ve and the cavitation number at the same fixed cross-section.
Presented theoretical results allow explaining the
experimental facts of both a weak and hysteresis dependence of the cavity length on ventilation and its abrupt increase.
Acknowledgment
The author thanks Professor Kai Yan for very useful discussions and his presentation of the paper on CAV2012.