MH 91 14.98% (mh91-il)
MH 91 14.98% - Martin Hepperle MH 91 parafoil
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(mh91-il) MH 91 14.98% Martin Hepperle MH 91 parafoil Max thickness 15% at 27.3% chord. Max camber 1.4% at 18.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 91 14.98% 1.00000000 0.00000000 0.99637709 0.00002958 0.98560583 0.00033179 0.96797278 0.00130687 0.94392791 0.00325155 0.91404829 0.00635118 0.87899752 0.01067586 0.83948856 0.01618388 0.79625113 0.02274051 0.75000721 0.03013431 0.70145495 0.03810479 0.65125857 0.04635928 0.60004517 0.05459757 0.54840347 0.06252258 0.49688650 0.06985746 0.44601357 0.07634937 0.39627394 0.08177882 0.34812910 0.08595855 0.30201551 0.08873420 0.25834725 0.08998063 0.21752060 0.08956605 0.17981541 0.08733741 0.14539007 0.08326657 0.11442362 0.07740992 0.08699607 0.06982190 0.06308235 0.06077159 0.04285220 0.05066826 0.02651514 0.03973019 0.01401516 0.02823397 0.00535870 0.01676100 0.00075455 0.00589881 0.00023515 0.00319922 0.00000161 0.00025423 0.00016384 -0.00250338 0.00050737 -0.00420642 0.00108933 -0.00574781 0.00200183 -0.00718564 0.00325259 -0.00862013 0.00563733 -0.01078105 0.00857643 -0.01295430 0.01791554 -0.01833880 0.03512557 -0.02558078 0.05721461 -0.03256363 0.08382298 -0.03912507 0.11460419 -0.04508585 0.14923387 -0.05027074 0.18739790 -0.05457236 0.22868976 -0.05790550 0.27274625 -0.06012365 0.31927545 -0.06122807 0.36782977 -0.06135131 0.41782671 -0.06053990 0.46875633 -0.05875849 0.52017532 -0.05608131 0.57153973 -0.05266990 0.62221551 -0.04862127 0.67162374 -0.04392720 0.71933639 -0.03860149 0.76498425 -0.03280316 0.80814182 -0.02678468 0.84834142 -0.02082527 0.88506832 -0.01521711 0.91778251 -0.01022606 0.94591748 -0.00611294 0.96883615 -0.00307613 0.98587226 -0.00116439 0.99641906 -0.00024324 1.00000000 0.00000000 |
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Polars for MH 91 14.98% (mh91-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh91-il | 50,000 | 9 | 16.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh91-il | 50,000 | 5 | 25.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh91-il | 100,000 | 9 | 34.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh91-il | 100,000 | 5 | 40.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh91-il | 200,000 | 9 | 52.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh91-il | 200,000 | 5 | 55.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh91-il | 500,000 | 9 | 78.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh91-il | 500,000 | 5 | 75.3 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh91-il | 1,000,000 | 9 | 96.6 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh91-il | 1,000,000 | 5 | 91.4 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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