Airfoil Tools
Search 1638 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

S4094 (root airfoil designed for and used on the E-flite UMX ASK-21 scale RC sailplane) (s4094-il)

S4094 (root airfoil designed for and used on the E-flite UMX ASK-21 scale RC sailplane) - Selig airfoil for micro RC soaring. Used on the E-flite UMX ASK-21 scale RC sailplane.


Airfoil s4094-il
Details Dat file Parser  
(s4094-il) S4094 (root airfoil designed for and used on the E-flite UMX ASK-21 scale RC sailplane)
Selig airfoil for micro RC soaring. Used on the E-flite UMX ASK-21 scale RC sailplane.
Max thickness 9.9% at 29.1% chord.
Max camber 1.8% at 33.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S4094 (root airfoil designed for and used on the E-flite UMX ASK-21 scale RC sailplane)
    1.000449559154914000  0.012413240564829640
    0.997089710528439200  0.012539654068309550
    0.987414057456497400  0.013332345894084180
    0.972102251362762500  0.014982614278941440
    0.951393991201984500  0.017139848038936890
    0.925399320878656100  0.019796293004748060
    0.894481572216979400  0.023028748222189090
    0.859097434916502000  0.026820839216479290
    0.819748574563173800  0.031127639086981000
    0.776977553042811300  0.035870075741750630
    0.731361370936399700  0.040949369759146490
    0.683501909563793600  0.046237302784324330
    0.634018878716784300  0.051587585809928550
    0.583540181911161700  0.056825820326860330
    0.532695105180941200  0.061755521304418060
    0.482115943659967300  0.066132654747350940
    0.432271086279200600  0.069582075011333480
    0.383478804879303600  0.071945148639956950
    0.336138592048056000  0.073215353653230880
    0.290693647039995200  0.073337252378080380
    0.247549819704092000  0.072261666269791360
    0.207072543663297000  0.069968227968713130
    0.169592710890196200  0.066456958894491330
    0.135393505771163500  0.061766194425731470
    0.104722419438493900  0.055959456383264540
    0.077772200349265910  0.049145888982014410
    0.054703707279801120  0.041465532581958580
    0.035615831554461460  0.033113531892814870
    0.020589208628665530  0.024331366888395380
    0.009635385925773289  0.015436627026914020
    0.002791878853425467  0.006859167013268561
    0.000028249230125121 -0.000683452410026169
    0.002609227544408510 -0.006616071896707050
    0.011161423518479490 -0.011608273281087740
    0.024908851864505090 -0.016044812634670260
    0.043788764809402860 -0.019689064297979060
    0.067699071498551260 -0.022519115845313610
    0.096481690660961340 -0.024560171981793450
    0.129883207726814600 -0.025884188510488290
    0.167584448763365000 -0.026553513946371690
    0.209194069252126100 -0.026668284445900760
    0.254238236611995600 -0.026308611804246780
    0.302240530785712600 -0.025495584973026180
    0.352730302907086700 -0.024332622110367860
    0.405127850959354700 -0.022996263588240170
    0.458777572640722900 -0.021574746832205770
    0.513021110552176500 -0.020140121449932480
    0.567197962460379100 -0.018740305739314120
    0.620652245542987900 -0.017421744821138820
    0.672738245416608800 -0.016213565413239570
    0.722827119210992900 -0.015146221525054400
    0.770312360333024500 -0.014234600943026380
    0.814616084067246500 -0.013494936402719440
    0.855194174282557500 -0.012927262525468440
    0.891541882530184500 -0.012531242615941140
    0.923198390076286700 -0.012286293903360480
    0.949747898525925300 -0.012161448064833260
    0.970865231144103200 -0.012054913757723900
    0.986436575938261300 -0.011964587820973000
    0.996204273163321100 -0.012167516296002620
    0.999568144188753600 -0.012382840516237100
Dat file parser warnings
  • Line 2 - X value too large but included: 1.000449559154914000 0.012413240564829640
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

S4095 (designed for the E-flite UMXPreviewDetails
S5010PreviewDetails
RG 14 10% AIRFOILPreviewDetails
MH 45 9.85%PreviewDetails
MH 60 10.08%PreviewDetails
M6 (85%)PreviewDetails
E221 (9.39%)PreviewDetails
RG 14 9.5% AIRFOILPreviewDetails
MH 44 9.66%PreviewDetails
MH 61 10.26%PreviewDetails

Polars for S4094 (root airfoil designed for and used on the E-flite UMX ASK-21 scale RC sailplane) (s4094-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s4094-il50,000929.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4094-il50,000534.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s4094-il100,000944.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4094-il100,000547.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   s4094-il200,000959.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s4094-il200,000558.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   s4094-il500,000976.5 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4094-il500,000573.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   s4094-il1,000,000987.8 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4094-il1,000,000582.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit