Case 19 :
Span = 3.048
Root Chord = 0.3048
Tip Chord = 0.3048
MAC = 0.3048
Reference Area = 0.929
Aspect Ratio = 10
Sweep Back = 35 Degrees
Twist = 0 Degree
Dihedral = 0 Degree
Number Of Chordwise Panels = 8 , Number Of Spanwise Panels = 32 , Uniformally Distributed Both Ways , Trailing Wakes Extended Downstream To A distance Of 100 Time The Mean Aerodynamic Chord In A direction Parallel To The Body X-Axis
Theoretical |
Airloads | Tornado | Surfaces |
XFLR5 |
|
---|---|---|---|---|---|
Lift Slope CL CD lift (Ibf) Drag (Ibf) Lift/Drag |
0.0748 0.748 0.0178 253 6 42 |
0.0715 0.7289 0.0181 246.8367 6.1441 40.175 |
0.07183 0.7289 0.01814 246.8371 6.144 40.175 |
0.07365 0.723 0.0166 245 5.6 43.5 |
---- 0.7255 0.0187 248.06 6.3939 38.797 |