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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)




NACA M2


New! Bulk download of polars in Excel format: m2.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.

−20−1001020−0.200.20.4
-45 deg deflection-35 deg deflection-25 deg deflection-15 deg deflection-5 deg deflection0 deg deflection5 deg deflection15 deg deflection25 deg deflection35 deg deflection45 deg deflectionNACA M2Plain flap effects from JavaFoil smooth airfoil data at Mach=0 and Re=6M, 40% flap chordSection lift coefficient vs angle of attackAngle of Attack (deg)Section Moment Coefficient c​m