RONCZ LOW DRAG FLYING WING AIRFOIL (marske7-il)
RONCZ LOW DRAG FLYING WING AIRFOIL - Roncz/Marske-7 low drag flying wing airfoil
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(marske7-il) RONCZ LOW DRAG FLYING WING AIRFOIL Roncz/Marske-7 low drag flying wing airfoil Max thickness 12.1% at 42.8% chord. Max camber 2.8% at 39.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
RONCZ LOW DRAG FLYING WING AIRFOIL
36.0 36.0
0.0000000 0.0000000
0.0013332 0.0051643
0.0049478 0.0104931
0.0128813 0.0177836
0.0268499 0.0266820
0.0483945 0.0367140
0.0756358 0.0463470
0.1069140 0.0550525
0.1403761 0.0625936
0.1751128 0.0690496
0.2105424 0.0744998
0.2463645 0.0790006
0.2824222 0.0825806
0.3186456 0.0852623
0.3549914 0.0870781
0.3913848 0.0880638
0.4276856 0.0882172
0.4637003 0.0874658
0.4992419 0.0856519
0.5342321 0.0825487
0.5688085 0.0779249
0.6033456 0.0716681
0.6383381 0.0638676
0.6742269 0.0548470
0.7111976 0.0451659
0.7479601 0.0358130
0.7841272 0.0273548
0.8200664 0.0199394
0.8560322 0.0136265
0.8924838 0.0084525
0.9280418 0.0047278
0.9548231 0.0029072
0.9717478 0.0022454
0.9833588 0.0020215
0.9924069 0.0019748
1.0000050 0.0020168
0.0000000 0.0000000
0.0003418 -.0023552
0.0023153 -.0056253
0.0065064 -.0086261
0.0145888 -.0117118
0.0300131 -.0151276
0.0547672 -.0185990
0.0865917 -.0216849
0.1219315 -.0241837
0.1586661 -.0261399
0.1959282 -.0276819
0.2334335 -.0289209
0.2710788 -.0299243
0.3088169 -.0307345
0.3466167 -.0313839
0.3844485 -.0318918
0.4222783 -.0322598
0.4600741 -.0324810
0.4978096 -.0325497
0.5354692 -.0324672
0.5730401 -.0322391
0.6105003 -.0318659
0.6478135 -.0313288
0.6849313 -.0305860
0.7218048 -.0295780
0.7584011 -.0282326
0.7947144 -.0264667
0.8307735 -.0241798
0.8665372 -.0212379
0.9014724 -.0175031
0.9326808 -.0132323
0.9564535 -.0093216
0.9722454 -.0064927
0.9834828 -.0044944
0.9923994 -.0030441
0.9999946 -.0020168
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Polars for RONCZ LOW DRAG FLYING WING AIRFOIL (marske7-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| marske7-il | 50,000 | 9 | 27.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 50,000 | 5 | 24 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 100,000 | 9 | 43.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 100,000 | 5 | 43.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 200,000 | 9 | 72 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 200,000 | 5 | 67.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 500,000 | 9 | 103.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 500,000 | 5 | 90.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 1,000,000 | 9 | 120.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 1,000,000 | 5 | 96.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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