NLR-7301 AIRFOIL (nlr7301-il)
NLR-7301 AIRFOIL - NLR NLR-7301 transonic airfoil
| Details | Dat file | Parser | |
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(nlr7301-il) NLR-7301 AIRFOIL NLR NLR-7301 transonic airfoil Max thickness 16.5% at 35% chord. Max camber 1.7% at 75% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
NLR-7301 AIRFOIL
40. 40.
0.0 0.000000
0.0005000 0.007300
0.0010000 0.010510
0.0020000 0.015180
0.0035000 0.020300
0.0050000 0.024240
0.0065000 0.027560
0.0080000 0.030430
0.0100000 0.033750
0.0125000 0.037290
0.0160000 0.041400
0.0200000 0.045140
0.0250000 0.048730
0.0350000 0.053720
0.0500000 0.059200
0.0650000 0.063210
0.0800000 0.066360
0.1000000 0.069850
0.1250000 0.073470
0.1500000 0.076480
0.2000000 0.081150
0.2500000 0.084410
0.3000000 0.086490
0.3500000 0.087550
0.4000000 0.087640
0.4500000 0.086780
0.5000000 0.084950
0.5500000 0.082060
0.6000000 0.077890
0.6500000 0.072120
0.7000000 0.064580
0.7500000 0.055510
0.8000000 0.045230
0.8500000 0.034150
0.9000000 0.022690
0.9250000 0.016960
0.9500000 0.011290
0.9750000 0.005770
0.9900000 0.002580
1.0000000 0.000550
0.0 0.000000
0.0005000 -0.007480
0.0010000 -0.010200
0.0020000 -0.013730
0.0035000 -0.017350
0.0050000 -0.020160
0.0065000 -0.022520
0.0080000 -0.024550
0.0100000 -0.026880
0.0125000 -0.029350
0.0160000 -0.032250
0.0200000 -0.035020
0.0250000 -0.037940
0.0350000 -0.042640
0.0500000 -0.048060
0.0650000 -0.052290
0.0800000 -0.055760
0.1000000 -0.059620
0.1250000 -0.063580
0.1500000 -0.066890
0.2000000 -0.071940
0.2500000 -0.075270
0.3000000 -0.077130
0.3500000 -0.077630
0.4000000 -0.076720
0.4500000 -0.074120
0.5000000 -0.069340
0.5500000 -0.062370
0.6000000 -0.053860
0.6500000 -0.043970
0.7000000 -0.033160
0.7500000 -0.022270
0.8000000 -0.012210
0.8500000 -0.004090
0.9000000 0.001080
0.9250000 0.002280
0.9500000 0.002460
0.9750000 0.001530
0.9900000 0.000420
1.0000000 -0.000550
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Polars for NLR-7301 AIRFOIL (nlr7301-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| nlr7301-il | 50,000 | 9 | 21 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlr7301-il | 50,000 | 5 | 18.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlr7301-il | 100,000 | 9 | 21.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlr7301-il | 100,000 | 5 | 26.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlr7301-il | 200,000 | 9 | 31 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlr7301-il | 200,000 | 5 | 37.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlr7301-il | 500,000 | 9 | 49.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlr7301-il | 500,000 | 5 | 55.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nlr7301-il | 1,000,000 | 9 | 67.1 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nlr7301-il | 1,000,000 | 5 | 70.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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