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Start Free Sprint →Standard Atmosphere model, Aircraft Anatomy (Fuselage, Wing, Empennage, Control Surfaces), Principles of Flight (Lift, Drag, Thrust, Weight), and Aircraft Instruments.
Key Points: Draw free body diagram. In steady level flight: Thrust = Drag (T = D) and Lift = Weight (L = W = 0.5 * rho * V^2 * S * C_L). Explain angle of attack alpha and stall condition.
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