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S8065 (11% version of S8064) (s8065-il)

S8065 (11% version of S8064) - Selig airfoil for Q-40 pylon racing (11%).


Airfoil s8065-il
Details Dat file Parser  
(s8065-il) S8065 (11% version of S8064)
Selig airfoil for Q-40 pylon racing (11%).
Max thickness 11% at 37.8% chord.
Max camber 1.1% at 56.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S8065 (11% version of S8064)
    1.000000000000000000  0.000000000000000000
    0.997993446185353500  0.000130811143500576
    0.992120253827858500  0.000648855829965359
    0.982560757808007100  0.001649265266565549
    0.969470785111610500  0.003248120022319079
    0.953091018839729800  0.005539948722110745
    0.933692440438248500  0.008559970954169636
    0.911573206720229500  0.012305217178092380
    0.887049593574342100  0.016722465320307010
    0.860448817703657600  0.021713525746054400
    0.832100105182719600  0.027125281982624930
    0.802327541350492800  0.032745884515611410
    0.771461468721389900  0.038191456467464470
    0.739364032839643000  0.043099196978347680
    0.705867124336291100  0.047496175047492290
    0.671223087933386800  0.051503637686130350
    0.635651228772872100  0.055096250743591880
    0.599356374311958400  0.058244507745990310
    0.562540327506452300  0.060902656670060410
    0.525412054459625100  0.063031440715143820
    0.488175880025791300  0.064604202196046630
    0.451018150627321500  0.065602106342505060
    0.414120232672516500  0.066002980976104590
    0.377671628557788000  0.065810184898614120
    0.341859321754045000  0.065052518633958320
    0.306879443495999200  0.063764173426503510
    0.272938389525968300  0.061971822234953300
    0.240236199932116400  0.059704693805376210
    0.208967271787325900  0.056988981021670270
    0.179314874520905800  0.053854515652283240
    0.151453252607483100  0.050333239885510120
    0.125546645934405500  0.046461822633340390
    0.101749367297932200  0.042275968248952310
    0.080199084935582920  0.037815310839931210
    0.061022939263114530  0.033125970468901500
    0.044340073838314400  0.028254618415642290
    0.030278750885406990  0.023237200132818140
    0.018886988472003760  0.018086935813106030
    0.010155978985443510  0.012834319451278800
    0.004107018662571682  0.007566208716775728
    0.000646005149050111  0.002533751850206041
    0.000317305124873490 -0.001759655920030518
    0.003478065414392439 -0.005841551016872853
    0.009658692195495977 -0.010229870203694930
    0.018626460148509990 -0.014558849261080630
    0.030372275245346030 -0.018719454442779120
    0.044882542651190520 -0.022634039186168460
    0.062078258938538470 -0.026259726942717550
    0.081881885564776710 -0.029582742697880410
    0.104195084088463100 -0.032595891466399000
    0.128893357330598000 -0.035285301807152790
    0.155824611427130000 -0.037651064424792120
    0.184818515012434100 -0.039685762243936630
    0.215688362938107800 -0.041377650120911770
    0.248240448135168900 -0.042708311083793540
    0.282271719146788600 -0.043663175631764720
    0.317570060249772200 -0.044216322387187220
    0.353937024770963400 -0.044339761347205520
    0.391177404913803600 -0.044027752558794460
    0.429082395421576500 -0.043268031629888480
    0.467455891409037800 -0.042063676179363250
    0.506121310618604900 -0.040456051085759100
    0.544861681056884400 -0.038502841063917010
    0.583408140717401600 -0.036261987650680670
    0.621492783639211900 -0.033749109561244770
    0.658833591251356300 -0.030943598854365060
    0.695330203156913700 -0.027700343754464280
    0.730996395498632300 -0.024137046831734080
    0.765632392092356900 -0.020573829589703380
    0.798917222729626100 -0.017161001071971070
    0.830542222261064500 -0.013997276597566710
    0.860207358743468800 -0.011150194673557670
    0.887625016401134900 -0.008656764763226560
    0.912524529935530300 -0.006531673974570347
    0.934655449683318200 -0.004763536039899971
    0.953787287593407700 -0.003312806807577075
    0.969755572684033700 -0.002082763468658889
    0.982533002695512700 -0.001038425611298955
    0.992036934495929800 -0.000321373691605693
    0.997972587516476600 -0.000026896364049739
    0.999999999999999800 -0.000000000000000039
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Polars for S8065 (11% version of S8064) (s8065-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s8065-il50,000931.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s8065-il50,000531.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s8065-il100,000949.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s8065-il100,000546.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s8065-il200,000969 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s8065-il200,000557.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   s8065-il500,000980.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   s8065-il500,000564.3 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s8065-il1,000,000988.8 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s8065-il1,000,000574.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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