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
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