5 1 Comparative study of topological charge 0 2 n a J 6 2 ] t YusukeNamekawa∗ a l CenterforComputationalSciences,UniversityofTsukuba,Tsukuba,Ibaraki305-8577,Japan - p E-mail: [email protected] e h [ Comparativestudy of topologicalcharge is performed. Topologicalchargesare measured by a 1 cloverleaf operator on smoothed gauge configurations. Various types of smoothing techniques v 5 are employed. Agreementof topologicalchargesin fermionic and gluonicdefinitions is exam- 9 ined.Highconsistencyisobservedbetweentopologicalchargesobtainedbyimprovedsmoothing 2 6 methodsandthosebytheindextheoremwiththeoverlap-Diracoperator. 0 . 1 0 5 1 : v i X r a The32ndInternationalSymposiumonLatticeFieldTheory, 23-28June,2014 ColumbiaUniversityNewYork,NY ∗Speaker. (cid:13)c Copyrightownedbytheauthor(s)underthetermsoftheCreativeCommonsAttribution-NonCommercial-ShareAlikeLicence. http://pos.sissa.it/ Comparativestudyoftopologicalcharge YusukeNamekawa 1. Introduction A topological charge is one of the most fundamental quantity in QCD. It characterizes the vacuum structure. Lattice QCD is a main tool in the study of the topological charge [1]. Lattice QCDallowsustoperformanonperturbative analysis inasystematic way. Thetopological charge isoften measured withagluonic fieldstrength operator onthelattice. Though it suffers from noisy ultraviolet fluctuations, a smoothing technique tames them so that a discernible signal of the topological charge can be obtained. Cooling or smearing have been used forsmoothinggaugefields. Recently,agradientflowisalsoemployed. Incontrasttothetraditional cooling and smearing, the gradient flow has an advantage that it provides a continuous change of thegaugefield. Thegradient flowaccomplishes abettercontrol ofsmoothing. Alternatively, the topological charge can be calculated with afermionic definition. Thetopo- logicalchargeisdetermined,forexample,bytheindextheoremwiththeoverlap-Diracoperator. A clearadvantageofthefermionicdefinitionisthattheresultisguaranteedtobeaninteger. Asubtle point, ontheotherhand,istheintegervaluesdependonthechoiceofthedefinition, duetoafinite lattice spacing. In the case of the overlap-Dirac operator, a value of the topological charge occa- sionallychangesaccordingtoaparameterintheformulation. Consistencycheckofthetopological charges in the fermionic and gluonic definitions would be helpful as an estimator of the scaling violation. In this work, topological charges are computed with gluonic operators on N = 2 topology f fixedgaugeconfigurations. Themeasurements areperformedusingseveralsmoothing techniques. Cooling with plaquette and improved local actions, APE and HYP smearing, as well as gradient flowsareemployed. Theresults arecompared witheachother, andwiththevalues obtained using theoverlap-Dirac operator. Similarattemptsarereported inRefs.[2]. 2. Setup 2.1 Gaugeconfiguration MeasurementofthetopologicalchargeisperformedonN =2gaugeconfigurationsprovided f byJLQCDCollaboration [3]. Thelatticesizeis163×32atthelatticespacingofa=0.118(2)fm. ThegluonactionisIwasaki-type improvedgaugeaction, Sg=b cg0 (cid:229) Pmn (x)+cg1 (cid:229) Rmn (x) , (2.1) x,m <n x,m ,n ! whereb =6/g2,cg=3.648, cg=−0.331. Thequarkactionisanoverlap-Dirac fermionaction, 0 0 1 S = q¯D (m)q, (2.2) q ov m m D (m) = m + + m − g sgn(H (−m )),H (−m )=g D (−m ), (2.3) ov 0 0 5 W 0 W 0 5 W 0 2 2 (cid:16) (cid:17) (cid:16) (cid:17) where m is the bare quark mass. D (−m ) is the Wilson operator with a negative mass, −m = W 0 0 −1.6. Furthermore, unphysical Wilson fermion y with a negative mass as well as twisted mass termsareaddedtofixthetopological chargedefinedbytheindextheorem Q , index d S =y¯D (−m )y +f †(D (−m )+img t )f , (2.4) W W 0 W 0 5 3 2 Comparativestudyoftopologicalcharge YusukeNamekawa b m Q #conf MDtime index 2.30 0.05 -2 50 2500 Table 1: Parameters of the gaugeconfigurations. Molecular Dynamics time is the numberof trajectories multipliedbythetrajectorylength. where f is a pseudofermion, and m is the twisted mass parameter. m = 0.2 is employed in the configuration generation. Each configuration is separated by 100 trajectories with its trajectory length0.5. Themainsimulationparameters aresummarizedinTable1. 2.2 Gluonictopological chargeoperator Thetopological chargeismeasured usingagluonic fieldstrength. Q = c Q1×1+c Q1×2, (2.5) improve 0 1 Q1×1,2 = 321p 2 (cid:229) e mnrs TrFmn1×1,2Frs1×1,2, (2.6) m ,n ,r ,s i 1 Fmn1×1,2 = − [Cm1n×1,2]AH,CmAn H = Cmn −Cm†n , (2.7) 4 2i (cid:0) (cid:1) where C1×1 is the cloverleaf constructed with 1×1 plaquettes, and C1×2 with 1×2 rectangular mn mn loops. The improvement coefficients c and c can be tuned to reduce the scaling violation in the 0 1 topological charge operator. Threetypesof(c ,c )areinvestigated. 0 1 (c ,c ) = (1,0) Naive-type, (2.8) 0 1 = (5/3,−1/12) Symanzik-type, (2.9) = (3.648,−0.331) Iwasaki-type. (2.10) Figure 1 displays c dependence of the topological charge on a single configuration smoothed by 1 Wilson flow. The topological charge with Symanzik-type coefficients has the smallest deviation from an integer. Since the deviation is originated from the finite lattice spacing, it implies an efficient reduction of the scaling violation by Symanzik-type operator. Calculations on other con- figurationsshowasimilartendency. Basedonthisresult,Symanzik-typecoefficientsareemployed inthiswork. 2.3 Smoothing Three kinds of smoothing techniques are evaluated: cooling, smearing, and gradient flow. Smoothingisrequiredtosuppressnoisyultraviolet fluctuations, whilekeepingatopological struc- ture. Although any smoothing is expected to give a consistent result in the continuum limit, it is valuable tofindamethodthathastheleastlatticeartifact. Coolingeliminatesultraviolet noisesbyreplacing eachlinkvariablesuchthatthelocalaction is minimized [4]. For the local action, not only a naive plaquette action, but also Symanzik and IwasakiactionsareemployedwiththecoefficientsofEq.(2.8)–(2.10). 3 Comparativestudyoftopologicalcharge YusukeNamekawa 0.20 163 · 32 e)| b = 2.30, mud = 0.050 v Qindex = -2 o 0.15 pr Wilson flow, t = 200 m Ntraj = 50 Qi nt( 0.10 e - i v Iwasaki o mpr 0.05 Naive Qi Symanzik | 0.00 -0.4 -0.35 -0.3 -0.25 -0.2 -0.15 -0.1 -0.05 0 0.05 c1 Figure1:Improvementcoefficientc dependenceofimprovedtopologicalchargeQ onasinglegauge 1 improve configuration.DifferenceofQ fromanintegerisplotted. improve Anotherwayofsmoothing issmearing. APEsmearing[5]isdefinedby a Umnew(x) = ProjSU(3) (1−a )Um (x)+ 6S m (x) ,a =0.6. (2.11) S m (x) = (cid:229) Un (hx)Um (x+n )Un†(x+m ) i (2.12) ±n 6=m Inaddition, HYPsmearing[6]isalsoexamined. a Umnew(x) = ProjSU(3) (1−a 1)Um (x)+ 61 (cid:229) Un(2;m)(x)Um(2;n)(x+n )Un(2,m),†(x+m ) , (2.13) " ±n 6=m # a Um(2;n)(x) = ProjSU(3) (1−a 2)Um (x)+ 42 (cid:229) Ur(3;mn) (x)Um(3;n)r (x+r )Ur(3,mn),†(x+m ) (,2.14) " ±r 6=m ,n # a Um(3;n)r (x) = ProjSU(3) (1−a 3)Um (x)+ 23 (cid:229) Us (x)Um (x+s )Us†(x+m ) , (2.15) " ±s 6=m ,n ,r # a = 0.75,a =0.6,a =0.3. (2.16) 1 2 3 Smearedgaugefieldsareprojected backtoSU(3)byMaximumSU(3)projection. ProjmaxSU(3)(Um (x)) = max ReTr(Umnew(x)Um†(x)). (2.17) SU(3) Umnew(x)∈SU(3) Analternative smoothing isgivenbythegradient flow[7]. Theevolution ofthegaugefieldis determined by ¶ S ¶ tVm (x,t) = −Vm (x,t)¶ Vm (x), (2.18) Vm (x,t =0) = Um (x), (2.19) where t is the flow time, and S is an action without its coupling constant. Similar to the cooling case, plaquette, Symanzik, and Iwasaki actions are employed. The flow equation is solved by the fourth order Runge-Kutta in the commutator-free method [8]. The Runge-Kutta step size dt is chosentobe0.02. Thesystematicerrorassociated withdiscretization oftheflowtimeisdefinitely belowthestatistical error. 4 Comparativestudyoftopologicalcharge YusukeNamekawa 2.0 163 · 32 Cooling(plaq) 2.0 163 · 32 Cooling(Symanzik) 2.0 163 · 32 Cooling(Iwasaki) 1.0 b = 2.30, mud = 0.050 1.0 b = 2.30, mud = 0.050 1.0 b = 2.30, mud = 0.050 Qindex = -2 Qindex = -2 Qindex = -2 0.0 0.0 0.0 mprove-1.0 mprove-1.0 mprove-1.0 Qi Qi Qi -2.0 -2.0 -2.0 -3.0 -3.0 -3.0 -4.00 50 100 150 200 250 300 -4.00 50 100 150 200 250 300 -4.00 50 100 150 200 250 300 Cooling step Cooling step Cooling step 2.0 163 · 32 APE 2.0 163 · 32 HYP 1.0 b = 2.30, mud = 0.050 1.0 b = 2.30, mud = 0.050 Qindex = -2 Qindex = -2 0.0 0.0 mprove-1.0 mprove-1.0 Qi Qi -2.0 -2.0 -3.0 -3.0 -4.00 100 200 300 400 500 600 -4.00 100 200 300 400 500 600 Smearing step Smearing step 2.0 163 · 32 Wilson flow 2.0 163 · 32 Symanzik flow 2.0 163 · 32 Iwasaki flow 1.0 b = 2.30, mud = 0.050 1.0 b = 2.30, mud = 0.050 1.0 b = 2.30, mud = 0.050 Qindex = -2 Qindex = -2 Qindex = -2 0.0 0.0 0.0 mprove-1.0 mprove-1.0 mprove-1.0 Qi Qi Qi -2.0 -2.0 -2.0 -3.0 -3.0 -3.0 -4.00 50 100 150 200 -4.00 50 100 150 200 -4.00 50 100 150 200 3 · flow time 3 · flow time 3 · flow time Figure2: SmoothingstepdependenceofQ usingcooling(toppanels),smearing(middlepanels),and improve gradientflow(bottompanels). 2.4 Results Figure2illustratescoolingandsmearingstepdependenceoftheimprovedtopologicalcharge. The flow time dependence is also plotted. The flow time is multiplied by a factor of three, which is expected from a perturbative analysis [9]. In every case, the topological charge has an integer value with a sufficiently large number of steps. A small number of smoothing steps leads to a fake plateau i.e. a semi-stable value of the topological charge. The number of smoothing steps is determinedtosatisfytheadmissibilitycondition, max[ReTr(1−U )]<0.067[10,11]. InFig.3, plaq Wilsonflowtimedependenceoftheplaquetteisshown. Nojumpofthetopologicalchargeseemto betriggered,iftheadmissibilityconditionisfulfilled. Itshouldbementionedmax[ReTr(1−U )] plaq doesnotalwaysdecreaseastheflowtimegrows,thoughthevaluesummedoverthespacetimefalls offmonotonically. Figure4presentshistogramsoftheimprovedtopologicalcharges. Sincethetopologicalcharge determinedbytheindexQ isfixedintheconfigurationgenerations,thehistogramisexpectedto index haveasharppeakaroundQ ,supposingthescalingviolationissmall. Thehistogramsobtained index by cooling withimproved local actions show the expected behavior. Almostall ofthe topological charges agree with Q . On the other hand, cooling using the plaquette action has a broad his- index togram. It implies a relatively large lattice artifact in the unimproved cooling method. Analogous trends are observed inother smoothing procedures. HYPsmearing has anarrow histogram, while APEsmearing does not. Symanzik and Iwasaki flowsform asharp peak inthe histogram. Onthe contrary, Wilson flow brings a wide peak. Improved smoothing methods leads to higher consis- 5 Comparativestudyoftopologicalcharge YusukeNamekawa 100 100 163 · 32 Wilson flow 163 · 32 Wilson flow 10 b = 2.30, mud = 0.050 10 b = 2.30, mud = 0.050 Qindex = -2 Qindex = -2 q) 1 1 a 1.0 - pl 00.0.11 0 - plaq 00.0.11 x( 1. a m 0.001 0.001 0.0001 0.0001 1e-05 1e-05 0 50 100 150 200 0 50 100 150 200 3 · flow time 3 · flow time Figure3: Wilsonflowtimedependenceofmaximumof(1−plaquette)(leftpanel),andthevaluesummed overthespacetimevolume(rightpanel). tency with Q , indicating the scaling violation in the topological charge is suppressed well by index theimprovement. 2.5 Conclusion Systematiccomparisonoftopologicalchargesispresented. Topologicalchargesaremeasured on N = 2 topology fixed configurations. Several smoothing techniques are evaluated using a f gluonictopologicalchargeoperatorofSymanzik-typecoefficients,whichgiveatopologicalcharge withthesmallestdeviation fromaninteger. Cooling with improved actions, HYPsmearing, and improved gradient flows are found to be advantageous. Morethan90%ofthetopological charges areconsistent withthoseobtained bythe indextheorem. Itindicates theirlatticeartifactsarereducedefficiently. Ontheotherhand,cooling with plaquette action, APE smearing, and Wilson flow lead to partial matches. The agreement is limitedto70-80%. Scalingviolations seemtobecomparatively largeinthesesmoothingmethods. Scaling properties as well as finite size effects of the topological charge have not been inves- tigated. It is important to estimate them, but is beyond the scope of this work due to limitation of thegaugeconfigurations. Thegaugeconfigurations havebeengenerated atasinglelatticespacing andspatial volume. Theseevaluations areleftforthefuturework. Acknowledgments I would like to thank members of MEXT SPIRE Field 5 Project 1 and Bridge++ develop- ment team, as well as H.Fukaya and K-I.Nagai for valuable discussions. I am grateful to JLQCD Collaboration forprovidingtheirgaugeconfigurations [3]. ThisworkisinpartbasedonBridge++ code[12,13,14]. ThisworkissupportedbyJLDGconstructedoverSINET3ofNII,MEXTSPIRE andJICFuS,andGrants-in-AidforScientificResearchGrantNumber24540250. References [1] Forarecentreview,seeM.Mueller-Preussker,PoS(LATTICE2014),003(2014). 6 Comparativestudyoftopologicalcharge YusukeNamekawa 50 163 · 32 Cooling(plaq) 50 163 · 32 Cooling(Symanzik) 50 163 · 32 Cooling(Iwasaki) 45 b = 2.30, mud = 0.050 45 b = 2.30, mud = 0.050 45 b = 2.30, mud = 0.050 40 Qindex = -2 40 Qindex = -2 40 Qindex = -2 35 35 35 30 30 30 25 25 25 20 20 20 15 15 15 10 10 10 5 5 5 0-6 -5 -4 -3 -2 -1 0 1 2 0-6 -5 -4 -3 -2 -1 0 1 2 0-6 -5 -4 -3 -2 -1 0 1 2 Qimprove Qimprove Qimprove 50 163 · 32 APE 50 163 · 32 HYP 45 b = 2.30, mud = 0.050 45 b = 2.30, mud = 0.050 40 Qindex = -2 40 Qindex = -2 35 35 30 30 25 25 20 20 15 15 10 10 5 5 0-6 -5 -4 -3 -2 -1 0 1 2 0-6 -5 -4 -3 -2 -1 0 1 2 Qimprove Qimprove 50 163 · 32 Wilson flow 50 163 · 32 Symanzik flow 50 163 · 32 Iwasaki flow 45 b = 2.30, mud = 0.050 45 b = 2.30, mud = 0.050 45 b = 2.30, mud = 0.050 40 Qindex = -2 40 Qindex = -2 40 Qindex = -2 35 35 35 30 30 30 25 25 25 20 20 20 15 15 15 10 10 10 5 5 5 0-6 -5 -4 -3 -2 -1 0 1 2 0-6 -5 -4 -3 -2 -1 0 1 2 0-6 -5 -4 -3 -2 -1 0 1 2 Qimprove Qimprove Qimprove Figure 4: Histograms of Q with cooling (top panels), smearing (middle panels), and gradient flow improve (bottompanels). 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