Upload
nguyendieu
View
213
Download
0
Embed Size (px)
Citation preview
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 1 >
Detached eddy simulation of
cloud cavitation on tip-modified propellers
Keun Woo Shin Propeller & Aftship R&D Department, MAN Diesel & Turbo
Frederikshavn, Denmark
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 2 >
Introduction – Cloud Cavitation (1)
Based on former publications
• Shin, K.W., Regener, P.B., Andersen, P., “Methods for cavitation prediction on tip-modified propellers in ship wake fields”, smp’15, Austin, USA, 2015
• Shin, K.W. and Andersen, P., “CFD analysis of cloud cavitation on three tip-modified propellers with systematically varied tip geometry”, 9th Int. Symp. on Cavitation, Lausanne, Switzerland, 2015
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 3 >
Introduction – Cloud Cavitation (2)
Cloud cavitation on ship propellers
• Intensive noise and mental surface erosion → Unacceptable for ship propellers
• Extensive sheet cavitation← High incident angle and low ambient pressure
• Sheet cavitation detachment← re-entrant jet (turbulent eddy)
• Periodic oscillations of incident angle
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 4 >
Introduction – Cloud Cavitation (3)
Cloud cavitation on ship propellers
• Leading-edge sheet cavitation extension in a high hull-wake region
← Incident angle increase and lowered hydrostatic pressure
• Detachment of sheet cavitation in a form of cloud cavitation
• Conversion of sheet cavitation into tip vortex cavitation
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 5 >
CFD Setup (1)
CFD solver
• STAR-CCM+® 9.02
• DES with k-ω SST turbulence model← Better prediction of detached cavitationthan RANS
• Imcompressible flow solver
• Volume of fluid (VOF) model
• Eulerian multiphase model
• Multiphase interaction→ Cavitation model based on Rayleigh-Plesset equation
• Gravity → Hydrostatic pressure
Cavitation estimations by RANS and DES
(Shin, K.W., (2014), “Cavitation simulation on Kappel
propeller with a hull wake field”, NuTTS2014, Marstrand,
Sweden )
RANS DES
40°
60°
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 6 >
CFD Setup (2)
CFD model
• Rotating domain around a propeller model with D=0.25 m
• Rigid body motion and sliding mesh
• Rudder model outside the rotating domain
• Trimmed hexahedral mesh
• Δx=0.5-1.0 mm on wall surface and Δx=0.1-0.5 mm on blade edge
• 6 prism layers and Δh=0.12-0.25 mm on wall surface → mostly y+≤1
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 7 >
CFD Setup (3)
CFD model
• Mesh refinement in region with sheetcavitation detachment← Volumetric control
• Unsteady computation with 1° propeller rotation per Δt → 116 μs > order of 10 μs for collectivebubble collapse duration← Practical indication of cloud cavitationrisk
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 8 >
CFD Setup (4)
Hull wake model
• Axial wake applied to velocity inletboundary located 3 propeller diameters upstream
• Transverse wake applied by usingmomentum source 1 propeller diameter upstream
Original
hull wake
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 9 >
CFD Setup (5)
Hull wake model
• Wake model test without a propeller model→ Accurate modeling of axial wake→ Characteristic bilge vortex→Deviation in modeling upward flow
Original
hull wake
Wake
model
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 10 >
Propeller models
Reference propeller
• 4-blade Kappel propeller with Ae/Ao=0.38
• Cavitation tunnel test showingextensive sheet & cloud cavitation
Two other propellers
• Modified from the reference propeller by varying tip loading
• Blade pitch variation → 10%, 35%, 60% tip pitch reduction
• Vertical incliation variation
0.6 0.8 1 1.2
0.4
0.6
0.8
1
s/R
P/D
Reference
High tip loading
Low tip loading
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 11 >
Cavitation simulations (1)
Validation against experimentresults
• Cavitation tunnel test with ship hullin SSPA, Gothenburg, Sweden
• Tunnel flow speed = 4.5 m/s, propeller speed = 24 rps, cavitation number = 3.8
• CFD cavitation interface of vaporvolume fraction = 0.1
• Cavitation starting at ϕ≈340°
• Sheet cavitation extention
Exp
CF
D
ϕ=340° 0° 20°
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 12 >
Cavitation simulations (2)
Validation against experimentresults
• Super-cavitation at 0.9R-1.0R
• Detachment of sheet cavitation
• Large structure of cloud cavitationin CFD ← Volume mesh of Δx≈0.5 mm
• Cavitation disappearance at ϕ≈90°E
xp
CF
D
ϕ=40° 60° 90°
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 13 >
Cavitation simulations (3)
High tip-loading propeller
• Sheet cavitation reduction at 0.7R-0.9R ← Lowered propeller speed by 0.5 rps
• Tip vortex cavitation (→0.5% lower propeller efficiency) and reduced cloud cavitation
Reference High tip-loading
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 14 >
Cavitation simulations (4)
Low tip-loading propeller
• Sheet cavitation increase ← Increased propeller speed by 0.5 rps
• Increased cloud cavitation
Reference Low tip-loading
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 15 >
Conclusion
Conclusion
• Steeply lowered tip loading→ Cloud cavitationon marine propellers
• Gradually lowered tip loading→ Prevention or reduction of cloud cavitation→ Propulsive efficiency lossfrom tip vortex
• Optimization of blade tip loadingin marine propeller design
• DES cavitation simulations → Practical tool for predictingcloud cavitation
ϕ=
40
°ϕ
=60
°
Reference
High
tip loading
Low
tip loading
• Hull wake modeling by velocity inlet & momentum source→ Effective way for applying hull wake without a hull model
07.03.2016© MAN Diesel & TurboDES of cloud cavitation on tip-modified propellers < 16 >
Thank You for Your Attention!
All data provided in this document is non-binding.
This data serves informational purposes only and is
especially not guaranteed in any way. Depending on the
subsequent specific individual projects, the relevant
data may be subject to changes and will be assessed and
determined individually for each project. This will depend
on the particular characteristics of each individual project,
especially specific site and operational conditions.