Horten 19.00% thick 3.00% camber
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Horten 19.00% thick 3.00% camber
Info
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DAT and DXF files
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Shape
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Venkataraman Fit
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Applications (0)
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Similarly shaped airfoils
Plain Flapped Shapes:
25% flap chord
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30% flap chord
|
35% flap chord
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40% flap chord
Basic Data:
c
l
vs α
|
c
d
vs α
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c
m
vs α
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c
l
/c
d
vs α
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c
d
vs c
l
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c
l
/c
d
vs c
l
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c
l
vs c
d
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c
m
vs c
l
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Curve fits
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Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects:
c
l
vs α
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c
d
vs α
|
c
m
vs α
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c
l
/c
d
vs α
|
c
d
vs c
l
|
c
l
/c
d
vs c
l
|
c
l
vs c
d
|
c
m
vs c
l
Roughness Effects:
c
l
vs α
|
c
d
vs α
|
c
m
vs α
|
c
l
/c
d
vs α
|
c
d
vs c
l
|
c
l
/c
d
vs c
l
|
c
l
vs c
d
|
c
m
vs c
l
Plain Flap Effects:
c
l,max
vs flap deflection:
all flap chords
|
25% flap chord
|
30% flap chord
|
35% flap chord
|
40% flap chord
Plain Flap Effects:
c
l
vs α for various flap deflections:
25% flap chord
|
30% flap chord
|
35% flap chord
|
40% flap chord
Plain Flap Effects:
c
m
vs α for various flap deflections:
25% flap chord
|
30% flap chord
|
35% flap chord
|
40% flap chord
Plain Flap Effects:
c
d
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.
Horten t/c=19.0%, f/c=3.0%
DB Name: Horten 19.00% thick 3.00% camber
Family:
Horten
Max thickness:
19.0% at x = 28.95% chord
Max camber:
2.2% at x = 24.57% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
XFOIL ncrit=9
Notes:
Coordinates generated by JavaFoil