BELL/WORTMANN FX 69-H-098 AIRFOIL (fx69h098-il)
BELL/WORTMANN FX 69-H-098 AIRFOIL - Bell/Wortmann FX 69-H-098 rotorcraft airfoil
| Details | Dat file | Parser | |
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(fx69h098-il) BELL/WORTMANN FX 69-H-098 AIRFOIL Bell/Wortmann FX 69-H-098 rotorcraft airfoil Max thickness 9.9% at 28.2% chord. Max camber 1.7% at 22.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
BELL/WORTMANN FX 69-H-098 AIRFOIL
23. 23.
0.0 0.0
0.00430 0.00960
0.00960 0.01480
0.01720 0.02040
0.03840 0.03200
0.05200 0.03770
0.08510 0.04860
0.12530 0.05730
0.17210 0.06300
0.22450 0.06610
0.28180 0.06660
0.34290 0.06540
0.40700 0.06310
0.47100 0.05980
0.53800 0.05530
0.60350 0.05010
0.66730 0.04420
0.72830 0.03770
0.78560 0.03120
0.83790 0.02480
0.88470 0.01850
0.95790 0.00720
1.00000 0.00090
0.00000 0.00000
0.00430 -0.00690
0.00960 -0.00960
0.01720 -0.01220
0.03840 -0.01710
0.05200 -0.01920
0.08510 -0.02310
0.12530 -0.02640
0.17210 -0.02920
0.22450 -0.03130
0.28180 -0.03230
0.34290 -0.03240
0.40700 -0.03170
0.47100 -0.03050
0.53800 -0.02880
0.60350 -0.02670
0.66730 -0.02420
0.72830 -0.02150
0.78560 -0.01860
0.83790 -0.01560
0.88470 -0.01260
0.95790 -0.00640
1.00000 -0.00130
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Polars for BELL/WORTMANN FX 69-H-098 AIRFOIL (fx69h098-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx69h098-il | 50,000 | 9 | 27.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69h098-il | 50,000 | 5 | 31.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69h098-il | 100,000 | 9 | 43.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69h098-il | 100,000 | 5 | 45.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69h098-il | 200,000 | 9 | 59.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69h098-il | 200,000 | 5 | 59.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69h098-il | 500,000 | 9 | 81.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69h098-il | 500,000 | 5 | 79 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69h098-il | 1,000,000 | 9 | 98.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69h098-il | 1,000,000 | 5 | 93.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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