Question: Q #1) Given: P (engine power) = 2x106 Watts, W (weight) = 56,000 lb, S (wing area) = 1000 ft, CD = 0.024 +0.04

Q #1) Given: P (engine power) = 2x106 Watts, W (weight) = 56,000 lb, S (wing area) = 1000 ft, CD = 0.024 +0.04 C2, p (air density) =8.8927e-04 slug/ft a) What is the cruise speed in ft/sec? b) What is the lift coefficient CL required? L c.g. T+ D W

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