USA-35B AIRFOIL (usa35b-il)
USA-35B AIRFOIL - USA-35B airfoil
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(usa35b-il) USA-35B AIRFOIL USA-35B airfoil Max thickness 11.6% at 30% chord. Max camber 4.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
USA-35B AIRFOIL
17.0 17.0
0.0000000 0.0000000
0.0125000 0.0239000
0.0250000 0.0335000
0.0500000 0.0476000
0.0750000 0.0589000
0.1000000 0.0669000
0.1500000 0.0780000
0.2000000 0.0852000
0.3000000 0.0900000
0.4000000 0.0866000
0.5000000 0.0757000
0.6000000 0.0605000
0.7000000 0.0432000
0.8000000 0.0226000
0.9000000 -.0004000
0.9500000 -.0126000
1.0000000 -.0251000
0.0000000 0.0000000
0.0125000 -.0173000
0.0250000 -.0213000
0.0500000 -.0248000
0.0750000 -.0262000
0.1000000 -.0269000
0.1500000 -.0276000
0.2000000 -.0270000
0.3000000 -.0261000
0.4000000 -.0250000
0.5000000 -.0237000
0.6000000 -.0231000
0.7000000 -.0234000
0.8000000 -.0241000
0.9000000 -.0256000
0.9500000 -.0264000
1.0000000 -.0276000
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Polars for USA-35B AIRFOIL (usa35b-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| usa35b-il | 50,000 | 9 | 24.6 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35b-il | 50,000 | 5 | 36.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35b-il | 100,000 | 9 | 53.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35b-il | 100,000 | 5 | 56.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35b-il | 200,000 | 9 | 76.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35b-il | 200,000 | 5 | 75.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35b-il | 500,000 | 9 | 106 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35b-il | 500,000 | 5 | 97 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35b-il | 1,000,000 | 9 | 125.6 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35b-il | 1,000,000 | 5 | 113.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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