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find D i and D p at (L/D) MAX: information we have is L = 10818 is the air density at sea level (approximately 0.002377
find Di and Dp at (L/D)MAX:
information we have is
L = 10818 is the air density at sea level (approximately 0.002377 slugs/ft)
V is the airspeed 425.85ft/s
S is the wing area (given as 227 ft)
C_L is the lift coefficient (given as 0.5)
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