Similarly shaped airfoils to NACA63A413
Direct link:
NACA63A413
Info
|
DAT and DXF files
|
Shape
|
Venkataraman Fit
|
Applications (1)
|
Similarly shaped airfoils
Plain Flapped Shapes:
25% flap chord
|
30% flap chord
|
35% flap chord
|
40% flap chord
Basic Data:
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
|
Curve fits
|
Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility 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
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.
1.
NACA64A413
2.
PSU-90-125WL
3.
NACA64-413 a=0.8
4.
NACA65-413 a=0.8
5.
NACA64-513
6.
NACA65-513
7.
GA 35A313
8.
MH 200 12.97%
9.
GA 37A313
10.
NACA63-413 a=0.8
11.
LS(1)-0413 (GA(W)-2)
12.
NACA64-414 a=0.8
13.
CB2513
14.
NACA65A413
15.
NACA64-514
16.
NACA63-513
17.
EPPLER 203
18.
GOE 548
19.
HN-956
20.
NACA64-413 a=0.6
21.
NACA63A414