TsAGI R-3a (12%) (tsagi-r-3a-il)
TsAGI R-3a (12%) - TsAGI R-3a used on Russian ultra light aircraft (12%).
| Details | Dat file | Parser | |
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(tsagi-r-3a-il) TsAGI R-3a (12%) TsAGI R-3a used on Russian ultra light aircraft (12%). Max thickness 12.1% at 23.1% chord. Max camber 3.1% at 24.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
TsAGI R-3a (12%)
1.000000 0.002000
0.995190 0.002632
0.987392 0.003658
0.978900 0.004777
0.969760 0.005986
0.960044 0.007274
0.949852 0.008628
0.939284 0.010037
0.928430 0.011488
0.917368 0.012969
0.906162 0.014474
0.894852 0.015997
0.883472 0.017531
0.872046 0.019076
0.860587 0.020627
0.849103 0.022184
0.837602 0.023746
0.826089 0.025312
0.814564 0.026881
0.803033 0.028453
0.791499 0.030027
0.779961 0.031602
0.768422 0.033179
0.756885 0.034755
0.745356 0.036331
0.733836 0.037908
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0.710800 0.041056
0.699274 0.042631
0.687747 0.044206
0.676219 0.045780
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0.653153 0.048924
0.641621 0.050494
0.630090 0.052060
0.618563 0.053625
0.607040 0.055187
0.595520 0.056745
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0.144183 0.090150
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0.107731 0.082582
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0.032725 0.048314
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0.022752 0.040115
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0.010014 0.025482
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0.000608 0.006962
0.000451 0.005678
0.000369 0.004404
0.000363 0.003136
0.000433 0.001873
0.000582 0.000613
0.000810 -0.000640
0.001123 -0.001876
0.001524 -0.003088
0.002020 -0.004267
0.002619 -0.005401
0.003331 -0.006479
0.004168 -0.007484
0.005140 -0.008405
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0.020856 -0.015326
0.022918 -0.015887
0.025121 -0.016397
0.027484 -0.016867
0.030026 -0.017318
0.032759 -0.017778
0.035688 -0.018268
0.038825 -0.018782
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0.053955 -0.020893
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0.068919 -0.022412
0.074779 -0.022858
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0.095549 -0.023938
0.103633 -0.024223
0.112287 -0.024483
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0.131113 -0.024912
0.141165 -0.025080
0.151562 -0.025219
0.162237 -0.025334
0.173130 -0.025429
0.184193 -0.025507
0.195373 -0.025575
0.206621 -0.025636
0.217885 -0.025688
0.229132 -0.025720
0.240359 -0.025725
0.251576 -0.025693
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0.274130 -0.025509
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0.319993 -0.024957
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0.354552 -0.024524
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0.400294 -0.023794
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0.434483 -0.023043
0.445900 -0.022755
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0.468791 -0.022131
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0.514779 -0.020736
0.526304 -0.020365
0.537835 -0.019985
0.549368 -0.019598
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0.572439 -0.018798
0.583976 -0.018386
0.595517 -0.017965
0.607056 -0.017537
0.618600 -0.017100
0.630146 -0.016655
0.641697 -0.016203
0.653251 -0.015742
0.664811 -0.015276
0.676371 -0.014803
0.687936 -0.014322
0.699506 -0.013835
0.711083 -0.013343
0.722660 -0.012845
0.734242 -0.012341
0.745827 -0.011833
0.757417 -0.011319
0.769010 -0.010801
0.780607 -0.010279
0.792206 -0.009752
0.803807 -0.009222
0.815408 -0.008689
0.827008 -0.008153
0.838603 -0.007614
0.850188 -0.007074
0.861757 -0.006532
0.873299 -0.005990
0.884799 -0.005448
0.896233 -0.004908
0.907569 -0.004372
0.918760 -0.003842
0.929743 -0.003321
0.940437 -0.002815
0.950746 -0.002326
0.960567 -0.001861
0.969800 -0.001424
0.978371 -0.001019
0.986233 -0.000648
0.991080 -0.000420
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Polars for TsAGI R-3a (12%) (tsagi-r-3a-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| tsagi-r-3a-il | 50,000 | 9 | 16.2 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 50,000 | 5 | 25.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 100,000 | 9 | 33 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 100,000 | 5 | 43.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 200,000 | 9 | 56.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 200,000 | 5 | 60.8 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 500,000 | 9 | 86.5 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 500,000 | 5 | 88.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 1,000,000 | 9 | 112.1 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 1,000,000 | 5 | 108.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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