saverrrr333

rrrr333  时间:2021-04-06  阅读:()
TutorialforXFoilDownloadXFoilDownloadXFoilfromhttp://raphael.
mit.
edu/xfoil/.
Itwouldbeagoodideatodownloadthedocumentationforfuturereferenceaswell.
InstallingXFoilCopythedownloadedfiletothedirectorywhereyouwanttoinstallXFoilandrunit.
RunningXfoilXFoilisexecutedbygoingtothedirectorywhereitwasinstalledandtyping%xfoilLoadinganAirfoilTheloadorNACAcommandcanusedtoloadanairfoilintoXFoil.
InthistutorialwewillbeusingaNACA2412airfoil.
ToloadthisairfoiltypeXFOILc>NACA2412NoticethatXFoilwillreturnsomeofthespecificationsfortheairfoil,includingthelocationandmagnitudeofthemaximumthickness,maximumcamber,andotherparameters.
CleaningtheAirfoilGeometryItisagoodideatoensurethattheairfoilloadeddoesnotcontainpanelsthatcreateverysharpedges.
ThePANEcommandinXFoilsmoothesouttheairfoilgeometry.
XFOILc>paneNOTE:ThecommandsarenotcasesensitiveTheOPERSub-LevelTypeXFOILc>OPERThiswillproducetheprompt.
OPERic>Typea""toseealistofavailablecommandsandabriefdescriptionoftheiruse.
ThisworksonanylevelofXFoil.
IntheOPERlevelthisiswhatyouwillseeaftertyping""ReturntoTopLevelRedolastALFA,CLI,CL,ASEQ,CSEQ,VELSViscrToggleInviscid/Viscousmode.
VPARChangeBLparameter(s)RerChangeReynoldsnumberMachrChangeMachnumberTypeiChangetypeofMach,RevariationwithCLITERChangeviscous-solutioniterationlimitINITToggleBLinitializationflagAlfarPrescribealphaCLIrPrescribeinviscidCLClrPrescribeCLASeqrrrPrescribeasequenceofalphasCSeqrrrPrescribeasequenceofCLsSEQPTogglepolar/Cp(x)sequenceplotdisplayCINCToggleminimumCpinclusioninpolarHINCTogglehingemomentinclusioninpolarPacciToggleautopointaccumulationtoactivepolarPGETfReadnewpolarfromsavefilePWRTiWritepolartosavefilePSUMShowsummaryofstoredpolarsPLISiListstoredpolar(s)PDELiDeletestoredpolarPSORiSortstoredpolarPPloii.
Plotstoredpolar(s)APloii.
Plotstoredairfoil(s)foreachpolarASETiCopystoredairfoilintocurrentairfoilPREMir.
Removepoint(s)fromstoredpolarPPAXChangepolarplotaxislimitsRGETfReadnewreferencepolarfromfileRDELiDeletestoredreferencepolarGRIDToggleCpvsxgridoverlayCREFTogglereferenceCpdataoverlayFREFTogglereferenceCL,CD.
.
datadisplayCPxPlotCpvsxCPVPlotairfoilwithpressurevectors(geewiz).
VPloBLvariableplots.
ANNOAnnotatecurrentplotHARDHardcopycurrentplotSIZErChangeplot-objectsizeCPMIrChangeminimumCpaxisannotationBLiPlotboundarylayervelocityprofilesBLCPlotboundarylayervelocityprofilesatcursorBLWTrChangevelocityprofilescaleweightFMOMCalculateflaphingemomentandforcesFNEWrrSetnewflaphingepointVELSrrCalculatevelocitycomponentsatapointDUMPfOutputUe,Dstar,Theta,Cfvss,x,ytofileCPWRfOutputxvsCptofileCPMNReportminimumsurfaceCpNAMEsSpecifynewairfoilnameNINCIncrementnameversionnumberNoticethattherearethreecolumns,thefirstisthecommand,thesecondonegivesanindicationofotherinputsthecommandneeds.
An"r"meansthatthecommandexpectsarealnumber,an"i"meansthatthecommandexpectsaninteger,an"f"meansthatthecommandexpectsafilename,andan"s"thatthecommandexpectsastring.
IftheinputisnottypedafterthecommandXFoilwillprompttheuser.
XFoilUnderInviscidModeNoticethe"i"nextto".
OPER"ontheprompt.
ThisindicatesthatXFoilisininviscidmode.
Type.
OPERic>alfa0XFoilwillfindtheflowaroundtheairfoilforthegivenangleofattack,inthiscase,0.
Noticethatawindowpopsupshowingthepressuredistribution,thesectionliftcoefficient,thesectionmomentcoefficient,theangleofattackandtheairfoilname.
Figure1.
CpDistributionatalpha=0Type.
OPERic>cl0.
7XFoilwillfindtheangleofattackatwhichthecurrentairfoilproducesthesectionliftcoefficientthathasbeeninput.
NoticethatXFoilonceagainplotsthepressuredistributionaroundtheairfoillikeitdidpreviously.
Figure2.
PressureDistrubionatCl=0.
6ViscousModeType.
OPERic>viscThiscommandwillturnontheviscousmode.
XFoilthenpromptstheusertoinputaReynoldsnumber.
ForthistutorialwewillworkwithalowReynoldsnumber,type"3e6"attheprompt.
Noticethata"v"willnowappearnextto"OPER"intheprompttoindicateviscousflow.
Tofindtheflowaroundtheairfoilatanangleofattackofzerodegreestype.
OPERvc>alfa0Noticethatnowthereseemtobetwopressuredistributions.
Thedashedlinesrepresenttheinviscidflowdistribution.
Thisprovidesaneasywaytocompareviscousandinviscidflow.
Figure3.
ViscousFlowAroundanAirfoilNoticealsothattheboundarylayerisoutlinedaroundtheairfoil.
Furthermore,thecoefficientofdragandthelift-to-dragratioarealsopresented.
Ifyoulookatthecommandscreen,thelastiterationalsoprovidesmoredataabouttheairfoil:Side1freetransitionatx/c=0.
527446Side2freetransitionatx/c=0.
3940386rms:0.
1349E-04max:0.
1462E-03Cat382a=0.
000CL=0.
2422Cm=-0.
0527CD=0.
00545=>CDf=0.
00466CDp=0.
00079Itprovidesthepointoftransitiontoturbulentflowintheupperandlowersurfaces.
ItalsoprovidesCDfandCDp,thefrictiondragandpressuredragrespectively.
GettingaHardCopyTogetacopyinpostscriptformatofthedisplayedplottype.
OPERvc>hardAcopywillbeproducedontheXFoildirectoryunderthefilenameplot.
ps.
YouwillnotbeabletoopenthisfileuntilyouexitXFoil.
However,anyotherfilesthatyouhardcopywillbeappendedtothefileplot.
ps.
ChangingthenumberofiterationsType.
OPERvc>alfa18YouwillnoticethatXFoildoesnotconverge.
Thisisbecauseitreachedthemaximumnumberofiterations.
Therearetwodifferentthingsthatcanbedone.
Type"!
",thiscommandwilltellXFoiltoiteratesomemore.
AsyoucanseeXFoilwillnotconvergeevenafteryoudothisonce.
Youcankeeptyping"!
"untilXFoilconvergesoryoucantrychangingthemaximumnumberofiterations.
Type.
OPERvc>iterApromptwillaskyoutoenterthenumberofiterations,type"100".
Thentype.
OPERvc>alfa18YouwillnoticethatXFoilwillconvergeafterabout54moreiterations.
ChangingtheCpminNoticethatatanangleofattackof18degreestheminimumCpislowerthan-2,thedefaultCpmin.
Type.
OPERvc>cpmnThiswilldisplaytheminimumCpdistributionMinimumInviscidCp=-17.
2591atx=0.
0004MinimumViscousCp=-12.
1387atx=0.
0010Type.
OPERvc>cpmi-18Tore-plottheCpdistributiontype.
OPERvc>cpxTheCpdistributionshouldnowlooklikethis:Figure4.
FlowAroundanAirfoilataHighAlphaSavingtheCpDistributiontoaFileType.
OPERvc>cpwrYouwillbepromptedtoenterafilename.
Enter"naca2412@18.
cp".
ThefilewillbesavedintextformatanditispossibletouseMATLABtoanalyzethedata.
RunningXFoilforaSeriesofAnglesofAttackType.
OPERvc>alfa0Then.
OPERvc>paccThiswillcreateafiletowhichthesectionliftcoefficient,thesectiondragcoefficient,theupperandlowertransitionpointsandotherdatawillbesaved.
Thiscommandalsoenablestheautopointaccumulation.
Youwillbepromptedtoenterafilenameforthenewlycreatedpolarfile.
Type"naca2412.
pol".
PressEnterwhenpromptedforapolardumpfilename.
Nowtype.
OPERvac>aseq020.
5ThiscommandwillrunXFoilforaseriesofanglesofattack,from0to20degreesat0.
5degreeincrements.
Type.
OPERvac>paccThiswillturnoffthepointaccumulation.
Thefile"naca2412.
pol"willbeinatextformatandcanbereadbyMATLAB.
ChangingthePointofTransitiontoTurbulentFlowType.
OPERvc>alfa0Thelastiterationwilllooklikethis:Side1freetransitionatx/c=0.
527446Side2freetransitionatx/c=0.
3940383rms:0.
8854E-04max:0.
1737E-02Cat382a=0.
000CL=0.
2422Cm=-0.
0527CD=0.
00545=>CDf=0.
00466CDp=0.
00079Noticeonthecommandwindowthatthepointoftransitionoftheuppersurface(Side1)isatx/c=0.
5274.
Letforcetransitionatx/c=0.
1.
Type.
OPERvc>vparThiscommandwillmoveyouintotheVPARsub-levelType.
.
VPARc>xtr0.
11Thiscommandwillforcetransitionatx/c=0.
1fortheuppersurfaceandx/c=1atthetopsurface(whichisthesameasfreetransition).
PressentertomovedowntotheOPERsub-level.
Type.
OPERvc>alfa0Thelastiterationwillnowlooklikethis:Side1forcedtransitionatx/c=0.
100022Side2freetransitionatx/c=0.
3824373rms:0.
6169E-05max:0.
1369E-03Cat372a=0.
000CL=0.
2238Cm=-0.
0499CD=0.
00763=>CDf=0.
00630CDp=0.
00133Noticethattransitionnowoccursatx/c=0.
1likeexpected.
Youcanalsoseethedifferenceinthesectiondragcoefficients.
QuittingXFoilPressenteruntilyoureturntothetoplevel,thentypeXFOILc>quit

HyperVMart:加拿大vps,2核/3G/25G NVMe/G口不限流量/季付$10.97,免费Windows系统

hypervmart怎么样?hypervmart是一家成立了很多年的英国主机商家,上一次分享他家还是在2年前,商家销售虚拟主机、独立服务器和VPS,VPS采用Hyper-V虚拟架构,这一点从他家的域名上也可以看出来。目前商家针对VPS有一个75折的优惠,而且VPS显示的地区为加拿大,但是商家提供的测速地址为荷兰和英国,他家的优势就是给到G口不限流量,硬盘为NVMe固态硬盘,这个配置用来跑跑数据非常...

SugarHosts糖果主机圣诞节促销 美国/香港虚拟主机低至6折

SugarHosts 糖果主机商我们算是比较熟悉的,早年学会建站的时候开始就用的糖果虚拟主机,目前他们家还算是为数不多提供虚拟主机的商家,有提供香港、美国、德国等虚拟主机机房。香港机房CN2速度比较快,美国机房有提供优化线路和普通线路适合外贸业务。德国欧洲机房适合欧洲业务的虚拟主机。糖果主机商一般是不会发布黑五活动的,他们在圣圣诞节促销活动是有的,我们看到糖果主机商发布的圣诞节促销虚拟主机低至6折...

御云(RoyalYun):香港CN2 GIA VPS仅7.9元每月起,美国vps仅8.9/月,续费同价,可叠加优惠

御云怎么样?炎炎暑期即将来临,御云(royalyun)香港、美国服务器开启大特惠模式。御云是新成立的云服务提供商,主要提供香港、美国的云服务器,不久将开启虚拟主机业务。我们的香港和美国主机采用CN2 GIA线路。目前,香港cn2 gia vps仅7.9元每月起,美国vps仅8.9/月,续费同价,可叠加优惠,香港云服务器国内延迟一般在50ms左右,是搭建网站的最佳选择,但是请不要用于违法用途。点击进...

rrrr333为你推荐
美国互联网瘫痪如果全球网络瘫痪3分钟会造成多少损失对对塔今儿老师给推荐了一个叫对对塔的学习网站,看起来挺不错的,有用过的人吗?管不管用?哪些功能比较好啊?甲骨文不满赔偿公司倒闭员工不满一年怎么赔偿百度关键词价格查询百度关键字如何设定竟价价格?曲妙玲张婉悠香艳版《白蛇传》是电影还是写真集?rawtoolsTF卡被写保护了怎么办?同ip网站一个域名能对应多个IP吗www.522av.com在白虎网站bhwz.com看电影要安装什么播放器?www.765.com下载小说地址m.2828dy.comwww.dy6868.com这个电影网怎么样?
虚拟主机空间 北京vps google镜像 电影服务器 mediafire 韩国加速器 iisphpmysql 512au 网站被封 anylink 工作站服务器 中国电信测速网 超级服务器 yundun 重庆电信服务器托管 主机管理系统 东莞主机托管 美国迈阿密 cdn服务 小夜博客 更多