EPPLER 904 AIRFOIL (e904-il)
EPPLER 904 AIRFOIL - Eppler E904 hydrofoil
| Details | Dat file | Parser | |
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(e904-il) EPPLER 904 AIRFOIL Eppler E904 hydrofoil Max thickness 9% at 44.9% chord. Max camber 1.3% at 50.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 904 AIRFOIL
56.0 54.0
0.0000000 0.0000000
0.0010800 0.0019200
0.0039900 0.0044000
0.0084900 0.0071600
0.0145400 0.0101100
0.0221100 0.0132000
0.0311500 0.0163800
0.0416300 0.0196200
0.0535200 0.0228700
0.0667700 0.0261100
0.0813400 0.0293000
0.0971900 0.0324300
0.1142500 0.0354600
0.1324900 0.0383700
0.1518200 0.0411200
0.1722200 0.0436600
0.1936700 0.0460000
0.2161000 0.0481400
0.2394400 0.0500900
0.2636000 0.0518500
0.2885200 0.0534100
0.3140900 0.0547700
0.3402500 0.0559200
0.3669000 0.0568500
0.3939400 0.0575600
0.4213000 0.0580400
0.4488800 0.0583000
0.4765900 0.0583200
0.5043400 0.0581100
0.5320200 0.0576500
0.5595600 0.0569400
0.5868500 0.0559900
0.6138100 0.0547700
0.6403400 0.0532900
0.6663500 0.0515100
0.6917600 0.0494400
0.7164400 0.0469400
0.7405400 0.0438600
0.7642700 0.0404200
0.7875000 0.0368700
0.8101000 0.0332900
0.8319200 0.0297800
0.8528300 0.0263700
0.8727200 0.0231200
0.8914700 0.0200400
0.9089500 0.0171500
0.9250800 0.0144500
0.9397500 0.0119500
0.9528700 0.0095900
0.9644300 0.0073100
0.9745200 0.0051200
0.9831400 0.0031800
0.9902100 0.0016500
0.9955200 0.0006300
0.9988600 0.0001200
1.0000000 0.0000000
0.0000000 0.0000000
0.0010700 -.0018000
0.0041300 -.0039800
0.0088200 -.0063100
0.0150800 -.0087000
0.0228700 -.0110900
0.0321500 -.0134300
0.0428700 -.0156300
0.0550500 -.0176100
0.0687800 -.0193600
0.0840300 -.0209500
0.1007400 -.0224200
0.1188500 -.0237700
0.1382800 -.0250200
0.1589600 -.0261500
0.1808200 -.0271800
0.2037800 -.0281100
0.2277600 -.0289300
0.2526600 -.0296400
0.2784100 -.0302600
0.3049100 -.0307600
0.3320700 -.0311600
0.3597900 -.0314600
0.3879800 -.0316500
0.4165300 -.0317300
0.4453400 -.0317000
0.4743100 -.0315600
0.5033500 -.0313100
0.5323400 -.0309500
0.5611900 -.0304800
0.5897900 -.0298900
0.6180500 -.0291800
0.6458600 -.0283400
0.6731300 -.0273800
0.6997500 -.0262800
0.7256300 -.0250300
0.7506800 -.0236100
0.7748000 -.0219700
0.7979700 -.0199800
0.8203600 -.0176100
0.8420400 -.0151100
0.8628700 -.0126800
0.8826900 -.0104000
0.9013600 -.0083100
0.9187400 -.0064700
0.9346900 -.0048800
0.9490900 -.0035200
0.9618600 -.0023400
0.9729700 -.0013600
0.9823500 -.0006100
0.9899000 -.0001500
0.9954500 0.0000400
0.9988500 0.0000400
1.0000000 0.0000000
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Polars for EPPLER 904 AIRFOIL (e904-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e904-il | 50,000 | 9 | 21.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e904-il | 50,000 | 5 | 24 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e904-il | 100,000 | 9 | 29.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e904-il | 100,000 | 5 | 41.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e904-il | 200,000 | 9 | 61.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e904-il | 200,000 | 5 | 53.9 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e904-il | 500,000 | 9 | 67.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e904-il | 500,000 | 5 | 72.4 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e904-il | 1,000,000 | 9 | 86.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e904-il | 1,000,000 | 5 | 87.7 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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