Delta Wing Aircraft Specifications (do the necessary assumptions if needed) Wing Area: 585 m2 Wing Span:...

Delta Wing Aircraft Specifications

(do the necessary assumptions if needed)

Wing Area: 585 m²

Wing Span: 32 m

Taper ratio: 0.019

Leading Edge Sweep angle: 65.57°

Wing loading: 4070 N/m²

Cruise Mach Number: 3

Cruise altitude: 22.5 km

(L/D) _cruise = (L/D) _max = 9

Calculate the cruising angle of attack?

Write down the cruising drag polar equation?

Using the drag polar found in (b), calculate (C_L^1/2/C_D) _max and corresponding Mach number maximizing (C_L^1/2/C_D).

Expert Solution

samet mamat answered 2 years ago

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