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NACA0006 (JF, WT, XF)
NACA0008 (JF, XF)
NACA0009 (JF, WT, XF)
NACA0010 (JF, XF)
NACA0012 (JF, WT, CFD, XF)
NACA0013 (JF, XF)
NACA0015 (JF, XF)
NACA0016 (JF, XF)
NACA0017 (JF, XF)
NACA0018 (JF, XF)
NACA0021 (JF, XF)
NACA0024 (JF, XF)
NACA0025 (JF, XF)
NACA0030 (JF, XF)
NACA1408 (JF, WT, XF)
NACA1409 (JF, XF)
NACA1410 (JF, WT, XF)
NACA1412 (JF, WT, XF)
NACA1415 (JF, XF)
NACA1418 (JF, XF)
NACA1420 (JF, XF)
NACA1421 (JF, XF)
NACA1424 (JF, XF)
NACA2.4511 (JF, WT, XF)
NACA2206 (JF, XF)
NACA2209 (JF, XF)
NACA2210 (JF, XF)
NACA2212 (JF, XF)
NACA2213 (JF, XF)
NACA2215 (JF, XF)
NACA2216 (JF, XF)
NACA2218 (JF, XF)
NACA2219 (JF, XF)
NACA2221 (JF, XF)
NACA2224 (JF, XF)
NACA2309 (JF, XF)
NACA2310 (JF, XF)
NACA2312 (JF, XF)
NACA2315 (JF, XF)
NACA2317 (JF, XF)
NACA2318 (JF, XF)
NACA2321 (JF, XF)
NACA2324 (JF, XF)
NACA2408 (JF, XF)
NACA2409 (JF, XF)
NACA2410 (JF, XF)
NACA2411 (JF, XF)
NACA2412 (JF, WT, XF)
NACA2414 (JF, WT, XF)
NACA2415 (JF, WT, XF)
NACA2416 (JF, XF)
NACA2417 (JF, XF)
NACA2418 (JF, WT, XF)
NACA2421 (JF, WT, XF)
NACA2424 (JF, WT, XF)
NACA3409 (JF, XF)
NACA3410 (JF, XF)
NACA3412 (JF, XF)
NACA3413 (JF, XF)
NACA3414 (JF, XF)
NACA3415 (JF, XF)
NACA3418 (JF, XF)
NACA3421 (JF, XF)
NACA4312 (JF, XF)
NACA4315 (JF, XF)
NACA4318 (JF, XF)
NACA4321 (JF, XF)
NACA4324 (JF, XF)
NACA4409 (JF, XF)
NACA4410 (JF, XF)
NACA4412 (JF, WT, XF)
NACA4413 (JF, XF)
NACA4415 (JF, WT, XF)
NACA4416 (JF, XF)
NACA4418 (JF, WT, XF)
NACA4421 (JF, WT, XF)
NACA4424 (JF, WT, XF)
NACA5509 (JF, XF)
NACA5510 (JF, XF)
NACA5512 (JF, XF)
NACA5514 (JF, XF)
NACA5515 (JF, XF)
NACA5518 (JF, XF)
NACA5521 (JF, XF)
NACA5524 (JF, XF)
NACA6209 (JF, XF)
NACA6210 (JF, XF)
NACA6212 (JF, XF)
NACA6215 (JF, XF)
NACA6218 (JF, XF)
NACA6221 (JF, XF)
NACA6224 (JF, XF)
NACA6409 (JF, WT, XF)
NACA6410 (JF, XF)
NACA6412 (JF, XF)
NACA6415 (JF, XF)
NACA6418 (JF, XF)
NACA6421 (JF, XF)
NACA6424 (JF, XF)




NACA66A419


New! Bulk download of polars in Excel format: NACA66A419.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

−1−0.500.511.5−0.12−0.1−0.08−0.06−0.04−0.020
Re 50k, JavaFoilRe 100k, JavaFoilRe 250k, JavaFoilRe 500k, JavaFoilRe 1M, JavaFoilRe 3M, JavaFoilRe 6M, JavaFoilRe 12M, JavaFoilRe 50k, XFOILRe 100k, XFOILRe 250k, XFOILRe 500k, XFOILRe 1M, XFOILRe 3M, XFOILRe 6M, XFOILRe 12M, XFOILNACA66A419Basic data from JavaFoil for smooth airfoil at Mach 0, and windtunnel data if availableSection moment coefficient vs section lift coefficientSection Lift Coefficient c​lSection Moment Coefficient c​m