MH 38 9.68% (mh38-il)
MH 38 9.68% - Martin Hepperle MH 38 for Endurance Model
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(mh38-il) MH 38 9.68% Martin Hepperle MH 38 for Endurance Model Max thickness 9.7% at 31.6% chord. Max camber 3.9% at 45.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
MH 38 9.68% 1.00000000 0.00000000 0.99681503 0.00052829 0.98744069 0.00206411 0.97219660 0.00461800 0.95140806 0.00820800 0.92548959 0.01281789 0.89490506 0.01838273 0.86016416 0.02479642 0.82181533 0.03191761 0.78043788 0.03956173 0.73663624 0.04751042 0.69102740 0.05547946 0.64418318 0.06313426 0.59661875 0.07011860 0.54875352 0.07607236 0.50090364 0.08072602 0.45336696 0.08391210 0.40640999 0.08556514 0.36036364 0.08573940 0.31562154 0.08448700 0.27256521 0.08186533 0.23156049 0.07795837 0.19296831 0.07288249 0.15714479 0.06675919 0.12440457 0.05971034 0.09500846 0.05189461 0.06919502 0.04351376 0.04717790 0.03479969 0.02915078 0.02601488 0.01528686 0.01746260 0.00575479 0.00948521 0.00235064 0.00541874 0.00111503 0.00342820 0.00031376 0.00160406 0.00004242 0.00050128 0.00003977 -0.00047153 0.00036581 -0.00138795 0.00098926 -0.00233639 0.00235538 -0.00378184 0.00418802 -0.00522915 0.00770050 -0.00733786 0.01930582 -0.01179167 0.03580768 -0.01540495 0.05722344 -0.01796634 0.08354806 -0.01940709 0.11472174 -0.01979314 0.15054213 -0.01929586 0.19065718 -0.01808367 0.23464739 -0.01630031 0.28202506 -0.01409517 0.33225215 -0.01160078 0.38474591 -0.00895640 0.43888457 -0.00628764 0.49401514 -0.00372487 0.54945063 -0.00138348 0.60447998 0.00063604 0.65838377 0.00226561 0.71044473 0.00346256 0.75997115 0.00422322 0.80630433 0.00456190 0.84883284 0.00452284 0.88699574 0.00415677 0.92028513 0.00353829 0.94826245 0.00274890 0.97054484 0.00186730 0.98678139 0.00099194 0.99667312 0.00027913 1.00000000 0.00000000 |
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Polars for MH 38 9.68% (mh38-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh38-il | 50,000 | 9 | 37.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 50,000 | 5 | 37.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 100,000 | 9 | 61.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 100,000 | 5 | 61.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 200,000 | 9 | 86.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 200,000 | 5 | 85.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 500,000 | 9 | 122.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 500,000 | 5 | 114.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 1,000,000 | 9 | 149.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 1,000,000 | 5 | 133.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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