MH 95 15.86% (mh95-il)
MH 95 15.86% - Martin Hepperle MH 95 parafoil
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(mh95-il) MH 95 15.86% Martin Hepperle MH 95 parafoil Max thickness 15.8% at 33.6% chord. Max camber 0.9% at 81.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 95 15.86% 1.00000000 0.00000000 0.99613463 0.00089175 0.98525133 0.00368100 0.96849335 0.00829916 0.94657783 0.01433614 0.92002417 0.02137586 0.88924640 0.02901834 0.85458309 0.03690385 0.81632849 0.04477352 0.77483401 0.05247457 0.73053846 0.05987315 0.68390550 0.06683561 0.63544809 0.07325957 0.58572205 0.07901097 0.53526323 0.08394066 0.48458283 0.08792380 0.43419484 0.09087208 0.38460973 0.09271123 0.33633074 0.09339292 0.28985022 0.09288191 0.24564576 0.09116145 0.20417934 0.08822440 0.16590012 0.08403888 0.13113128 0.07852833 0.10005118 0.07175734 0.07293327 0.06395791 0.05023285 0.05520734 0.03212292 0.04523379 0.01819093 0.03404712 0.00816384 0.02225781 0.00209172 0.01048013 0.00000796 -0.00061143 0.00264019 -0.00967365 0.01131284 -0.01725366 0.02603613 -0.02476388 0.04594663 -0.03208292 0.07062714 -0.03903295 0.09970541 -0.04545496 0.13279922 -0.05116084 0.16960433 -0.05594167 0.20985646 -0.05973603 0.25314594 -0.06256784 0.29899844 -0.06439753 0.34696906 -0.06521703 0.39652627 -0.06507526 0.44709454 -0.06395938 0.49811163 -0.06185897 0.54899576 -0.05871106 0.59929429 -0.05438810 0.64872662 -0.04888129 0.69702471 -0.04238377 0.74385415 -0.03520856 0.78879968 -0.02775361 0.83135926 -0.02045543 0.87092428 -0.01376861 0.90679840 -0.00809418 0.93819221 -0.00380110 0.96416369 -0.00111008 0.98369391 0.00005140 0.99586173 0.00013530 1.00000000 0.00000000 |
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Polars for MH 95 15.86% (mh95-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh95-il | 50,000 | 9 | 29.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh95-il | 50,000 | 5 | 29 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh95-il | 100,000 | 9 | 44.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh95-il | 100,000 | 5 | 37.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh95-il | 200,000 | 9 | 48.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh95-il | 200,000 | 5 | 45.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh95-il | 500,000 | 9 | 62.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh95-il | 500,000 | 5 | 60.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh95-il | 1,000,000 | 9 | 78 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh95-il | 1,000,000 | 5 | 74.3 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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