The design parameters of your wing are as follows: Mid-chord (or shock) Mach num...
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The design parameters of your wing are as follows:
Mid-chord (or shock) Mach number: 0.7
Cruise Mach number: 0.86
Aspect ratio: 8.59
'Uncranked' taper ratio λu: 0.42
Crank extent ηc: 0.22
Crank sweep λc: 8 degrees
Enter your mid-chord sweep angle to the nearest 0.1 degree:
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