EPPLER 874 HYDROFOIL AIRFOIL (e874-il)
EPPLER 874 HYDROFOIL AIRFOIL - Eppler E874 hydrofoil
| Details | Dat file | Parser | |
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(e874-il) EPPLER 874 HYDROFOIL AIRFOIL Eppler E874 hydrofoil Max thickness 7.9% at 28.8% chord. Max camber 0.9% at 35.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 874 HYDROFOIL AIRFOIL
61. 60.
0.0001900 0.0009700
0.0018000 0.0031100
0.0047600 0.0055000
0.0090000 0.0080300
0.0145000 0.0106900
0.0212100 0.0134200
0.0291000 0.0162000
0.0381400 0.0190100
0.0483100 0.0218200
0.0595800 0.0246000
0.0719100 0.0273300
0.0852700 0.0299900
0.0996200 0.0325700
0.1149300 0.0350400
0.1311400 0.0373800
0.1482200 0.0395800
0.1661300 0.0416100
0.1848000 0.0434500
0.2042000 0.0450800
0.2242600 0.0464700
0.2449400 0.0476000
0.2661800 0.0483900
0.2879900 0.0487700
0.3104400 0.0487300
0.3335400 0.0483600
0.3572300 0.0477300
0.3814500 0.0468700
0.4061200 0.0458100
0.4311800 0.0445800
0.4565500 0.0432000
0.4821700 0.0416900
0.5079500 0.0400800
0.5338200 0.0383800
0.5597100 0.0366200
0.5855300 0.0348100
0.6112000 0.0329600
0.6366400 0.0311000
0.6617800 0.0292400
0.6865400 0.0273900
0.7108200 0.0255600
0.7345700 0.0237600
0.7577000 0.0220000
0.7801400 0.0202800
0.8018200 0.0186300
0.8226500 0.0170300
0.8425900 0.0154900
0.8615500 0.0140200
0.8794800 0.0126100
0.8963301 0.0112700
0.9120200 0.0099900
0.9265200 0.0087600
0.9397800 0.0075900
0.9517400 0.0064500
0.9623800 0.0053200
0.9716900 0.0041500
0.9797600 0.0029500
0.9866300 0.0018300
0.9922500 0.0009300
0.9964600 0.0003400
0.9991000 0.0000600
1.0000000 0.0000000
0.0001900 0.0009700
0.0002300 -.0010200
0.0019100 -.0031500
0.0049000 -.0054700
0.0091600 -.0078900
0.0146500 -.0103800
0.0213100 -.0128800
0.0291300 -.0153500
0.0380700 -.0177700
0.0481100 -.0200900
0.0592000 -.0222600
0.0713300 -.0242500
0.0844700 -.0259600
0.0987000 -.0273200
0.1140900 -.0284200
0.1305800 -.0292900
0.1481400 -.0299600
0.1667200 -.0304500
0.1862700 -.0307600
0.2067500 -.0309100
0.2280900 -.0309000
0.2502500 -.0307600
0.2731600 -.0304900
0.2967600 -.0301000
0.3209800 -.0296100
0.3457600 -.0290200
0.3710200 -.0283400
0.3967000 -.0275900
0.4227200 -.0267800
0.4490100 -.0259200
0.4754800 -.0250000
0.5020600 -.0240600
0.5286700 -.0230800
0.5552400 -.0220800
0.5816800 -.0210800
0.6079200 -.0200600
0.6338700 -.0190500
0.6594700 -.0180400
0.6864200 -.0170400
0.7092600 -.0160600
0.7333100 -.0150900
0.7566900 -.0141500
0.7793400 -.0132300
0.8011900 -.0123300
0.8221700 -.0114500
0.8422200 -.0106000
0.8612700 -.0097700
0.8792700 -.0089700
0.8961599 -.0081800
0.9118900 -.0074000
0.9264200 -.0066300
0.9396900 -.0058700
0.9516600 -.0050900
0.9623100 -.0042800
0.9716300 -.0033800
0.9797200 -.0024000
0.9866101 -.0014700
0.9922300 -.0007200
0.9964600 -.0002500
1.0000000 0.0000000
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Polars for EPPLER 874 HYDROFOIL AIRFOIL (e874-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e874-il | 50,000 | 9 | 30.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e874-il | 50,000 | 5 | 29.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e874-il | 100,000 | 9 | 41.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e874-il | 100,000 | 5 | 40.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e874-il | 200,000 | 9 | 51.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e874-il | 200,000 | 5 | 49.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e874-il | 500,000 | 9 | 65.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e874-il | 500,000 | 5 | 60.7 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e874-il | 1,000,000 | 9 | 75 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e874-il | 1,000,000 | 5 | 63.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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