9 Empennage General Design - HAW Hamburg
9 - 4 Critical flight states for the empennage dimensioning from the point of view of control are: • Horizontal tailplane: critical combination of center-of-gravity position, flap position and airspeed; rotation during take-off; flare when landing: control with trimmed horizontal sta-bilizer (CS 25.255). • Vertical tailplane (fin): Engine failure in cruise and during take-off and landing.
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