S4095 (designed for the E-flite UMX ASK-21 scale RC sailplane) (s4095-il)
S4095 (designed for 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.
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(s4095-il) S4095 (designed for 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 9.7% at 29.1% chord. Max camber 1.7% at 33.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
S4095 (designed for the E-flite UMX ASK-21 scale RC sailplane)
1.000709986856786000 0.019435561869618120
0.997381299873247200 0.019454465881674130
0.987802796876802300 0.019992150447237440
0.972655665369400100 0.021369925002658730
0.952167454205606000 0.023210785698959820
0.926431386253521400 0.025496234869249390
0.895792419113741700 0.028297381583375740
0.860687336367940100 0.031596223805031710
0.821597313919953400 0.035351318117821570
0.779044930859798200 0.039491686850266580
0.733588940744883500 0.043931748289645500
0.685815718129041200 0.048560458832934930
0.636333164486872600 0.053252988969780790
0.585761815850116800 0.057859370401076160
0.534728548159155700 0.062211368469533270
0.483866087030270900 0.066098905488185210
0.433683382798542500 0.069205668599109940
0.384571359205225400 0.071370057897416960
0.336958185475575500 0.072529130004221010
0.291283249110267300 0.072605664326276480
0.247950827830073900 0.071535661283765980
0.207324589764900700 0.069286684961206450
0.169732629446199800 0.065848304558893120
0.135455046002508500 0.061249716732942220
0.104735138552667000 0.055545897219928930
0.077761203486294120 0.048838771106638240
0.054688554343579330 0.041261221586515160
0.035610117316996930 0.033003010000016120
0.020599521583571260 0.024299698297538760
0.009659754440131451 0.015465379696522250
0.002818631778016556 0.006924973811694069
0.000022589380155091 -0.000614114456619778
0.002505853760900956 -0.006516152716943195
0.010923499428699970 -0.011406232746411210
0.024556406266324160 -0.015683049419848250
0.043365625363226860 -0.019124166162342230
0.067265560971844440 -0.021727876416084500
0.096110283729180410 -0.023540027233240910
0.129653241223461800 -0.024656349593812560
0.167578572451644100 -0.025162379138777890
0.209495557525853600 -0.025186503638559380
0.254931157454820800 -0.024840242419386480
0.303366327277323000 -0.024222533243679310
0.354238483806599900 -0.023437706661127910
0.406921344334338400 -0.022586761212858610
0.460760551661784800 -0.021723923313906470
0.515100136336811200 -0.020893665057098270
0.569285682871087500 -0.020120896813080120
0.622670350882838200 -0.019433296908917740
0.674619818721198100 -0.018843846601201550
0.724518283637474700 -0.018370855110803520
0.771773384554371900 -0.018019440882473820
0.815821846853038600 -0.017799846973249250
0.856134135696300500 -0.017708363234551460
0.892219500657564000 -0.017744268568505950
0.923630100459782400 -0.017888626392159690
0.949961774517666900 -0.018114993820065940
0.970898091905129100 -0.018329233063205570
0.986326445373818700 -0.018535593056296980
0.995993122572240500 -0.019017708941027420
0.999319053505976700 -0.019349368687047420
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Polars for S4095 (designed for the E-flite UMX ASK-21 scale RC sailplane) (s4095-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| s4095-il | 50,000 | 9 | 27.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 50,000 | 5 | 32.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 100,000 | 9 | 41.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 100,000 | 5 | 43.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 200,000 | 9 | 53.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 200,000 | 5 | 53.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 500,000 | 9 | 67.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 500,000 | 5 | 65.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 1,000,000 | 9 | 75.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 1,000,000 | 5 | 72.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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