Math Problem Statement

If the aircraft in question 3 has a lift to drag ratio of 20 in cruise, determine the thrust required to maintain steady level cruise.

Solution

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Math Problem Analysis

Mathematical Concepts

Flight Mechanics

Formulas

Lift-to-Drag Ratio (L/D) = L/D = 20
Thrust Required (T) = D = W / (L/D)

Theorems

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Suitable Grade Level

Advanced