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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

 

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