CLARK Y AIRFOIL (clarky-il)
Details: Dat file: Parser (clarky-il) CLARK Y AIRFOIL CLARK Y airfoil Max thickness 11.7% at 28% chord. Max camber 3.4% at 42% chord Source UIUC Airfoil Coordinates Database Source dat file
CLARK-Y 11.7% smoothed (clarkysm-il) - Airfoil Tools
(clarkysm-il) CLARK-Y 11.7% smoothed CLARK Y airfoil (smoothed) Max thickness 11.7% at 30.9% chord. Max camber 3.5% at 43.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format
Airfoil plotter (clarky-il)
Plot and print the shape of an airfoil (aerofoil) for your specific chord width and transformation. The dat file data can either be loaded from the airfoil database or your own airfoils which can be entered here and they will appear in the list of airfoils in the form below.
CLARK Y AIRFOIL (clarky-il) Xfoil prediction polar at RE=100,000 …
Polar details for airfoil (aerofoil)CLARK Y AIRFOIL(clarky-il) Xfoil prediction at Reynolds number 100,000 and Ncrit 9
Airfoil database search
Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.
CLARK YM-15 AIRFOIL (clarym15-il)
(clarym15-il) CLARK YM-15 AIRFOIL CLARK YM15 airfoil Max thickness 15% at 29.6% chord. Max camber 3.6% at 39.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format: CLARK YM-15 AIRFOIL 17. 17.
Airfoil Tools
clark y airfoil 1.000000 0.000599 0.990000 0.002969 0.980000 0.005333 0.970000 0.007687 0.960000 0.010023 0.940000 0.014624 0.920000 0.019116 0.900000 0.023502 0.880000 0.027789 0.860000 0.031974 0.840000 0.036054 0.820000 0.040024 0.800000 0.043884 0.780000 0.047628 0.760000 0.051257 0.740000 0.054767 0.720000 0.058160 0.700000 …
CLARK X AIRFOIL (clarkx-il)
(clarkx-il) CLARK X AIRFOIL CLARK X airfoil Max thickness 11.7% at 30% chord. Max camber 3.3% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format: CLARK X AIRFOIL 17. 17.
Airfoil database list(C) c141a-il to clarky-il
Alphabetic list of airfoils (aerofoils) (C). LOCKHEED C-141 BL0 AIRFOIL to CLARK Y AIRFOIL
Airfoil Tools
clark y airfoil 61. 61. 0.000000 0.000000 0.000500 0.002339 0.001000 0.003727 0.002000 0.005803 0.004000 0.008924 0.008000 0.013735 0.012000 0.017858 0.020000 0.025374 0.030000 0.033022 0.040000 0.039128 0.050000 0.044275 0.060000 0.048757 0.080000 0.056431 0.100000 0.062998 0.120000 0.068620 0.140000 0.073436 0.160000 0.077571 …