LWK 79-100 (lwk79100-il)
LWK 79-100 - LWK 79-100 symmetrical airfoil
| Details | Dat file | Parser | |
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(lwk79100-il) LWK 79-100 LWK 79-100 symmetrical airfoil Max thickness 10% at 27.9% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
LWK 79-100 1.00000 0.00000 0.99893 0.00007 0.99572 0.00028 0.99039 0.00063 0.98296 0.00113 0.97347 0.00175 0.96194 0.00251 0.94844 0.00339 0.93301 0.00439 0.91573 0.00550 0.89668 0.00670 0.87592 0.00799 0.85355 0.00939 0.82967 0.01091 0.80438 0.01260 0.77779 0.01450 0.75000 0.01664 0.72114 0.01905 0.69134 0.02171 0.66072 0.02464 0.62941 0.02779 0.59755 0.03109 0.56526 0.03443 0.53270 0.03762 0.50000 0.04054 0.46730 0.04310 0.43474 0.04524 0.40245 0.04699 0.37059 0.04835 0.33928 0.04933 0.30866 0.04989 0.27886 0.04997 0.25000 0.04961 0.22221 0.04886 0.19562 0.04777 0.17033 0.04630 0.14645 0.04447 0.12408 0.04225 0.10332 0.03968 0.08427 0.03675 0.06699 0.03348 0.05156 0.02990 0.03806 0.02606 0.02653 0.02201 0.01704 0.01782 0.00961 0.01341 0.00428 0.00883 0.00107 0.00434 0.00000 0.00000 0.00107 -0.00434 0.00428 -0.00883 0.00961 -0.01341 0.01704 -0.01782 0.02653 -0.02201 0.03806 -0.02606 0.05156 -0.02990 0.06699 -0.03348 0.08427 -0.03675 0.10332 -0.03968 0.12408 -0.04225 0.14645 -0.04447 0.17033 -0.04630 0.19562 -0.04777 0.22221 -0.04886 0.25000 -0.04961 0.27886 -0.04997 0.30866 -0.04989 0.33928 -0.04933 0.37059 -0.04835 0.40245 -0.04699 0.43474 -0.04524 0.46730 -0.04310 0.50000 -0.04054 0.53270 -0.03762 0.56526 -0.03443 0.59755 -0.03109 0.62941 -0.02779 0.66072 -0.02464 0.69134 -0.02171 0.72114 -0.01905 0.75000 -0.01664 0.77779 -0.01450 0.80438 -0.01260 0.82967 -0.01091 0.85355 -0.00939 0.87592 -0.00799 0.89668 -0.00670 0.91573 -0.00550 0.93301 -0.00439 0.94844 -0.00339 0.96194 -0.00251 0.97347 -0.00175 0.98296 -0.00113 0.99039 -0.00063 0.99572 -0.00028 0.99893 -0.00007 1.00000 0.00000 |
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Polars for LWK 79-100 (lwk79100-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| lwk79100-il | 50,000 | 9 | 25.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 50,000 | 5 | 27.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk79100-il | 100,000 | 9 | 37.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 100,000 | 5 | 35.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk79100-il | 200,000 | 9 | 47.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 200,000 | 5 | 44.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk79100-il | 500,000 | 9 | 59.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 500,000 | 5 | 60.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lwk79100-il | 1,000,000 | 9 | 72.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lwk79100-il | 1,000,000 | 5 | 74.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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