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SAE
SAE AS81366A
Действует
Boundary Layer Control System; Pressure
Описание
Изменения
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Версии
This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.
Тематика
Maintainability and supportability
Electronic control systems
Human factors