2024年3月14日发(作者:子车焱)
JournalofFluidsandStructures40(2013)42–51
ContentslistsavailableatSciVerseScienceDirect
JournalofFluidsandStructures
journalhomepage:/locate/jfs
Largeeddysimulationofvortexsheddingandpressure
fluctuationinaerostaticbearings
JinchengZhu
a
,HanChen
a,b
,XuedongChen
a,
n
StateKeyLaboratoryofDigitalManufacturingEquipmentandTechnology,HuazhongUniversityofScienceandTechnology,
Wuhan430074,China
b
DepartmentofMechanics,HuazhongUniversityofScienceandTechnology,Wuhan430074,China
a
articleinfo
Articlehistory:
Received21May2012
Accepted5March2013
Availableonline28April2013
Keywords:
Aerostaticbearing
Largeeddysimulation
Vortexshedding
Pressurefluctuation
Vibration
abstract
Inaerostaticbearings,highspeedairflowmayinducesmallvibration,whichhasbeen
harmfultotheimprovementofmovingandpositioningaccuracyofaerostatically
paper,thetransientflowfield
intheaerostaticbearingisnumericallyinvestigatedusingthelargeeddysimulation
entstructuresarestudiedandvortexsheddingphenomenonisdiscovered
putationalresultsdemonstratethatvortexsheddingcauses
onshipbetweenpressurefluctuation
andbearingvibrationisestablishedbasedonoursimulationresultsandexperimentally
measuredvibrationstrength.
&htsreserved.
uction
Aerostaticbearingshahemeritof
near-zerofrictionandlowheatgeneration,applicationsofaerostaticbearingsmakeitpossibleforsupporteddevicesto
r,withtheincreasingdemandofpositioningaccuracy,theinherentsmall
vibrationontheorderofnanometers(Kawaietal.,2005)severelydamagesstabilityandprecisionofthebearing,especially
rstandandeventuallysuppressthisharmfulvibration,traditionaldesign
andanalysismethodsformassflowrateandloadcarryingcapacitydonotsufficeanymore,andlotsofresearcheffortshave
beenmadeontheairflowfieldinaerostaticbearings.
Recently,therelationshipbetweenthehighspeedairflowandthesmallvibrationinaerostaticbearingshasbeen
tal.(2005)studiedthenano-vibrationinultra-precisionmachinetoolsandattributed
dHe(2006)foundvortexflowstructuresinthebearingrecess
bycomputationalfluiddynamics(CFD)simulationofthesteadyairflowfield,andsuggestedthattheseairvorticesare
etal.(2006)alsoobservedthisairvortexflowbyCFD
simulationandreachedasimilarconclusion,andaccordinglyproposedanewrestrictordesigntoweakenthevibration.
Zhangetal.(2007)analyzedthehighReynoldsnumber(Re)flowinthebearingclearance,andreducedthevibrationof
entwork,Yoshimuraetal.(2012)attributednano-vibrationofaerostatic
bearingswithsurfacerestrictiontoghthe
flow-inducednatureofbearingvibrationhasgenerallybeenrecognized,thepreviousworksonlyassumedasteadyflow
n
./fax:+862787557325.
E-mailaddress:chenxd@().
0889-9746/$-seefrontmatter&htsreserved.
/10.1016/structs.2013.03.012
l./JournalofFluidsandStructures40(2013)42–5143
Nomenclature
d
0
d
1
d
2
h
_
m
p
r
r
0
r
1
r
2
t
u
i
,u
j
,u
k
orificediameter
recessdiameter
bearingdiameter
airfilmthickness
massflowrate
pressure
radialdistance
orificeradius
recessradius
bearingradius
time
flowvelocitiesinvariousdirections
x
i
,x
j
,x
k
z
H
P
0
P
s
P
A
Re
T
Δt
δ
ij
μ
ρ
s
ij
τ
ij
coordinatesinvariousdirections
verticaldistance
recessdepth
atmospherepressure
airsupplypressure
area-weightedaveragedpressure
Reynoldsnumber
temperature
timestepsize
Kroneckerdeltafunction
airviscosity
airdensity
molecularviscositystresstensor
subgrid-scalestress
fieldoraveragedtheflowfieldinaReynoldsAveragedNavier–Stokes(RANS)hisflow-inducedvibrationis
apparentlyatimedependentprocess,timedependentisnecessarytoinvestigatethetransientairflowfieldinthebearing
clearanceinordertofurtherunderstandthisharmfulsmallvibration.
Tonumericallyanalyzethedetailedflowcharacteristicsinaerostaticbearings,thefullNavier–Stokesequationsfor
hehighspeedairflowinthebearinggapneartheorificeoutletisturbulent,
RANSsimulationisusuallyemployed,andnumericalresultsdemonstrateadequateaccuracyinpredictingmeanflow
characteristics(ChenandHe,2006;LiandDing,2007).Pressuredepressions(Eleshaky,2009;Yoshimotoetal.,2007)and
vortexflowstructures(Chenetal.,2011)r,
RANSsimulationadoptsastatisticy,direct
numericalsimulation(DNS)canresolvethewholespectrumofturbulentscalesasnoturbulentmodelisassumed,butits
eeddysimulation(LES),largescaleturbulenteddiesaresolveddirectlyand
,coherentturbulentstructurescanbeobtainedwith
acceptablecomputationalcostinLES,whichhasbeenvalidatedinvariousapplications(Chengetal.,2012;Lametal.,2010;
Tucker,2011).
Inapreviousstudy(Chenetal.,2011),steadyRANSsimulationmethodwasusedtostudyairflowfieldsinvarious
aerostaticbearingswithdifferentparametersandrecessshapes,andtherelationshipbetweenvortexstrengthandvibration
r,notransientflowcharacteristicsintheaerostaticbearingcouldberesolved.
Inthispaper,theulationresultsreveal
ionofthebearingisalsomeasuredexperimentally,
anditisdemonstratedthatvibrationstrengthofthebearingincreaseswithincreasingpressurefluctuationinducedby
vortexsheddinginthebearingrecess.
calmodeling
InLES,largeeddiesofturbulencearedirectlyresolvedandeddieswithscalessmallerthangridspacingaremodeled.
ThegoverningequationsemployedinLESarethetime-dependentFavreFilteredNavier–Stokesequations,including
continuityandmomentumequations:
∂ρ∂
~
i
Þ¼0;
þ
ðρ
u
∂t∂x
i
~
ij
∂∂∂p
∂s
∂
~
i
Þþ
~
i
u
~
j
Þ¼−ðρ
u
ðρ
u
þ−ðτ~
ij
Þ;
∂t∂x
j
∂x
i
∂x
j
∂x
j
ð1Þ
ð2Þ
theFavrefilteristhedensity-weightedfilter,wheredensityandpressurearespatialfiltered(denotedby“
–
”)whilevelocity
isdensity-weighted(
e
üρÃ=ρ,
n
denotesageneralvariable).InEq.(2),s
ij
istheviscousstresstensorandτ
ij
isthesubgrid-
scale(SGS)stress,whicharedefinedas
2024年3月14日发(作者:子车焱)
JournalofFluidsandStructures40(2013)42–51
ContentslistsavailableatSciVerseScienceDirect
JournalofFluidsandStructures
journalhomepage:/locate/jfs
Largeeddysimulationofvortexsheddingandpressure
fluctuationinaerostaticbearings
JinchengZhu
a
,HanChen
a,b
,XuedongChen
a,
n
StateKeyLaboratoryofDigitalManufacturingEquipmentandTechnology,HuazhongUniversityofScienceandTechnology,
Wuhan430074,China
b
DepartmentofMechanics,HuazhongUniversityofScienceandTechnology,Wuhan430074,China
a
articleinfo
Articlehistory:
Received21May2012
Accepted5March2013
Availableonline28April2013
Keywords:
Aerostaticbearing
Largeeddysimulation
Vortexshedding
Pressurefluctuation
Vibration
abstract
Inaerostaticbearings,highspeedairflowmayinducesmallvibration,whichhasbeen
harmfultotheimprovementofmovingandpositioningaccuracyofaerostatically
paper,thetransientflowfield
intheaerostaticbearingisnumericallyinvestigatedusingthelargeeddysimulation
entstructuresarestudiedandvortexsheddingphenomenonisdiscovered
putationalresultsdemonstratethatvortexsheddingcauses
onshipbetweenpressurefluctuation
andbearingvibrationisestablishedbasedonoursimulationresultsandexperimentally
measuredvibrationstrength.
&htsreserved.
uction
Aerostaticbearingshahemeritof
near-zerofrictionandlowheatgeneration,applicationsofaerostaticbearingsmakeitpossibleforsupporteddevicesto
r,withtheincreasingdemandofpositioningaccuracy,theinherentsmall
vibrationontheorderofnanometers(Kawaietal.,2005)severelydamagesstabilityandprecisionofthebearing,especially
rstandandeventuallysuppressthisharmfulvibration,traditionaldesign
andanalysismethodsformassflowrateandloadcarryingcapacitydonotsufficeanymore,andlotsofresearcheffortshave
beenmadeontheairflowfieldinaerostaticbearings.
Recently,therelationshipbetweenthehighspeedairflowandthesmallvibrationinaerostaticbearingshasbeen
tal.(2005)studiedthenano-vibrationinultra-precisionmachinetoolsandattributed
dHe(2006)foundvortexflowstructuresinthebearingrecess
bycomputationalfluiddynamics(CFD)simulationofthesteadyairflowfield,andsuggestedthattheseairvorticesare
etal.(2006)alsoobservedthisairvortexflowbyCFD
simulationandreachedasimilarconclusion,andaccordinglyproposedanewrestrictordesigntoweakenthevibration.
Zhangetal.(2007)analyzedthehighReynoldsnumber(Re)flowinthebearingclearance,andreducedthevibrationof
entwork,Yoshimuraetal.(2012)attributednano-vibrationofaerostatic
bearingswithsurfacerestrictiontoghthe
flow-inducednatureofbearingvibrationhasgenerallybeenrecognized,thepreviousworksonlyassumedasteadyflow
n
./fax:+862787557325.
E-mailaddress:chenxd@().
0889-9746/$-seefrontmatter&htsreserved.
/10.1016/structs.2013.03.012
l./JournalofFluidsandStructures40(2013)42–5143
Nomenclature
d
0
d
1
d
2
h
_
m
p
r
r
0
r
1
r
2
t
u
i
,u
j
,u
k
orificediameter
recessdiameter
bearingdiameter
airfilmthickness
massflowrate
pressure
radialdistance
orificeradius
recessradius
bearingradius
time
flowvelocitiesinvariousdirections
x
i
,x
j
,x
k
z
H
P
0
P
s
P
A
Re
T
Δt
δ
ij
μ
ρ
s
ij
τ
ij
coordinatesinvariousdirections
verticaldistance
recessdepth
atmospherepressure
airsupplypressure
area-weightedaveragedpressure
Reynoldsnumber
temperature
timestepsize
Kroneckerdeltafunction
airviscosity
airdensity
molecularviscositystresstensor
subgrid-scalestress
fieldoraveragedtheflowfieldinaReynoldsAveragedNavier–Stokes(RANS)hisflow-inducedvibrationis
apparentlyatimedependentprocess,timedependentisnecessarytoinvestigatethetransientairflowfieldinthebearing
clearanceinordertofurtherunderstandthisharmfulsmallvibration.
Tonumericallyanalyzethedetailedflowcharacteristicsinaerostaticbearings,thefullNavier–Stokesequationsfor
hehighspeedairflowinthebearinggapneartheorificeoutletisturbulent,
RANSsimulationisusuallyemployed,andnumericalresultsdemonstrateadequateaccuracyinpredictingmeanflow
characteristics(ChenandHe,2006;LiandDing,2007).Pressuredepressions(Eleshaky,2009;Yoshimotoetal.,2007)and
vortexflowstructures(Chenetal.,2011)r,
RANSsimulationadoptsastatisticy,direct
numericalsimulation(DNS)canresolvethewholespectrumofturbulentscalesasnoturbulentmodelisassumed,butits
eeddysimulation(LES),largescaleturbulenteddiesaresolveddirectlyand
,coherentturbulentstructurescanbeobtainedwith
acceptablecomputationalcostinLES,whichhasbeenvalidatedinvariousapplications(Chengetal.,2012;Lametal.,2010;
Tucker,2011).
Inapreviousstudy(Chenetal.,2011),steadyRANSsimulationmethodwasusedtostudyairflowfieldsinvarious
aerostaticbearingswithdifferentparametersandrecessshapes,andtherelationshipbetweenvortexstrengthandvibration
r,notransientflowcharacteristicsintheaerostaticbearingcouldberesolved.
Inthispaper,theulationresultsreveal
ionofthebearingisalsomeasuredexperimentally,
anditisdemonstratedthatvibrationstrengthofthebearingincreaseswithincreasingpressurefluctuationinducedby
vortexsheddinginthebearingrecess.
calmodeling
InLES,largeeddiesofturbulencearedirectlyresolvedandeddieswithscalessmallerthangridspacingaremodeled.
ThegoverningequationsemployedinLESarethetime-dependentFavreFilteredNavier–Stokesequations,including
continuityandmomentumequations:
∂ρ∂
~
i
Þ¼0;
þ
ðρ
u
∂t∂x
i
~
ij
∂∂∂p
∂s
∂
~
i
Þþ
~
i
u
~
j
Þ¼−ðρ
u
ðρ
u
þ−ðτ~
ij
Þ;
∂t∂x
j
∂x
i
∂x
j
∂x
j
ð1Þ
ð2Þ
theFavrefilteristhedensity-weightedfilter,wheredensityandpressurearespatialfiltered(denotedby“
–
”)whilevelocity
isdensity-weighted(
e
üρÃ=ρ,
n
denotesageneralvariable).InEq.(2),s
ij
istheviscousstresstensorandτ
ij
isthesubgrid-
scale(SGS)stress,whicharedefinedas