UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sfm-il)
UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT - University of Alberta/Marsden UA 79-SF-187 sailplane airfoil MAIN ELEMENT
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(ua79sfm-il) UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT University of Alberta/Marsden UA 79-SF-187 sailplane airfoil MAIN ELEMENT Max thickness 18.8% at 42.8% chord. Max camber 3% at 66.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT
30.0 21.0
0.000000 0.000000
0.002400 0.005600
0.009500 0.015800
0.021200 0.027900
0.037500 0.040000
0.058100 0.052400
0.082800 0.064400
0.111200 0.076000
0.143100 0.086800
0.178100 0.096700
0.215800 0.105500
0.255600 0.112900
0.297300 0.119100
0.340200 0.123900
0.383900 0.127400
0.427800 0.129300
0.471500 0.129900
0.514500 0.128900
0.556100 0.126500
0.596000 0.122900
0.633600 0.117100
0.668600 0.110500
0.700500 0.101600
0.729000 0.092400
0.753600 0.082900
0.774200 0.075000
0.790500 0.068500
0.802300 0.063900
0.809400 0.061200
0.811700 0.060300
0.000000 0.000000
0.002400 -.003400
0.009500 -.008900
0.021200 -.014700
0.037500 -.020500
0.058100 -.026300
0.082800 -.031800
0.111200 -.037100
0.143100 -.041900
0.178100 -.046200
0.215800 -.049900
0.255600 -.053000
0.297300 -.055300
0.340200 -.057100
0.383900 -.058100
0.427800 -.058400
0.471500 -.057700
0.514500 -.056100
0.556100 -.053400
0.596000 -.049500
0.633600 -.042400
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Polars for UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN ELEMENT (ua79sfm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ua79sfm-il | 50,000 | 9 | 12.2 at α=17.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 50,000 | 5 | 16.3 at α=14.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sfm-il | 100,000 | 9 | 41.3 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 100,000 | 5 | 40.2 at α=11° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sfm-il | 200,000 | 9 | 82.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 200,000 | 5 | 80 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sfm-il | 500,000 | 9 | 145.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 500,000 | 5 | 142.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ua79sfm-il | 1,000,000 | 9 | 291 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ua79sfm-il | 1,000,000 | 5 | 241.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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