Case 9 :
Root Airfoil : NACA 23012 , Tip Airfoil : NACA 23012
Span = 6
Root Chord = 1
Tip Chord = 1
MAC = 1
Reference Area = 6
Aspect Ratio = 6
Sweep Back = 0 Degrees
Twist = 0 Degrees
Dihedral = 0 Degrees
Alpha |
Wind Tunnel
|
Airloads 1 x 20 |
Tornado 1 x 20 |
Airloads 8 x 24 |
Tornado 8 x 24
|
XFLR5 8 x 24 |
USAF-Datcom |
|---|---|---|---|---|---|---|---|
-4 |
-0.2000 -0.0700 0.0900 0.2450 0.4000 0.5500 0.7000 0.8400 1.0000 1.1500 1.2900 1.4100 1.5400 1.6100 1.5000 |
-0.2056 -0.0553 0.0952 0.2455 0.3951 0.5436 0.6907 0.8359 0.9789 1.1192 1.2566 1.3906 1.5210 1.6475 1.7699 |
-0.2048 -0.0545 0.0958 0.2461 0.3958 0.5443 0.6914 0.8366 0.9795 1.1199 1.2573 1.3913 1.5217 1.6482 1.7706 |
-0.2085
-0.0577 0.0933 0.2441 0.3943 0.5434 0.6910 0.8367 0.9801 1.1209 1.2586 1.3930 1.5237 1.6505 1.7730 |
-0.2080
-0.0572 0.0938 0.2446 0.3948 0.5439 0.6914 0.8372 0.9805 1.1213 1.2591 1.3934 1.5242 1.6509 1.7735 |
-0.2244 -0.0737 0.0774 0.2283 0.3782 0.5265 0.6726 0.8157 0.9554 1.0909 1.2219 1.3478 1.4680 1.5824 1.6904 |
-0.2120 -0.0640 0.0780 0.2280 0.3870 0.5520 0.7230 0.8970 1.0750 1.2370 1.3570 1.4500 1.5090 1.5300 1.3670 |