RG 14 9% AIRFOIL (rg149-il)
RG 14 9% AIRFOIL - Rolf Girsberger RG 14 (9%) airfoil
| Details | Dat file | Parser | |
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(rg149-il) RG 14 9% AIRFOIL Rolf Girsberger RG 14 (9%) airfoil Max thickness 9% at 31% chord. Max camber 1.6% at 36% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
RG 14 9% AIRFOIL
30. 30.
0.0000000 0.0000000
0.0046500 0.0097800
0.0144700 0.0177800
0.0293800 0.0254800
0.0493100 0.0326800
0.0741200 0.0392500
0.1036300 0.0450900
0.1375600 0.0498900
0.1755900 0.0542400
0.2173000 0.0574900
0.2622700 0.0596000
0.3099800 0.0605700
0.3598900 0.0604500
0.4114400 0.0592800
0.4640100 0.0571700
0.5170100 0.0542100
0.5697900 0.0505500
0.6217500 0.0463300
0.6722700 0.0416900
0.7207300 0.0367800
0.7668900 0.0317000
0.8105700 0.0265700
0.8512100 0.0215400
0.8881100 0.0167500
0.9206300 0.0123300
0.9481700 0.0083900
0.9702600 0.0048900
0.9865400 0.0021000
0.9965900 0.0004700
1.0000000 0.0000000
0.0000000 0.0000000
0.0046500 -.0064000
0.0144700 -.0114000
0.0293800 -.0158900
0.0493100 -.0197700
0.0741200 -.0229700
0.1036300 -.0255200
0.1375600 -.0274100
0.1755900 -.0287100
0.2173000 -.0294300
0.2622700 -.0296500
0.3099800 -.0294300
0.3598900 -.0287900
0.4114400 -.0278100
0.4640100 -.0265300
0.5170100 -.0249800
0.5697900 -.0232000
0.6217500 -.0211800
0.6722700 -.0189500
0.7207300 -.0163500
0.7668900 -.0132500
0.8105700 -.0099600
0.8512100 -.0069500
0.8881100 -.0044400
0.9206300 -.0025200
0.9481700 -.0011900
0.9702600 -.0003400
0.9865400 0.0000600
0.9965900 0.0000700
1.0000000 0.0000000
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Polars for RG 14 9% AIRFOIL (rg149-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| rg149-il | 50,000 | 9 | 33.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg149-il | 50,000 | 5 | 34.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg149-il | 100,000 | 9 | 48.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg149-il | 100,000 | 5 | 46.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg149-il | 200,000 | 9 | 63.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg149-il | 200,000 | 5 | 57.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg149-il | 500,000 | 9 | 81.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg149-il | 500,000 | 5 | 70.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg149-il | 1,000,000 | 9 | 90 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg149-il | 1,000,000 | 5 | 84.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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