Engine Inoperative Flight Principles, Zero Sideslip(엔진 부작동 비행 원리, 제로 사이드 슬립)

Engine Inoperative Flight Principles Best single-engine climb performance is obtained at ① VYSE with ② maximum available power and ③ minimum drag. After the ⅰ) flaps and landing gear have been retracted and the ⅱ) propeller of the failed engine feathered, a key element in best climb performance is ⅲ) minimizing sideslip. With a single-engine airplane or a multiengine airplane with both engines operative, sideslip is eliminated when the ball of the turn and bank instrument is centered. This is a condition of zero sideslip, and the airplane is presenting its smallest possible profile to th..........

원문링크 : Engine Inoperative Flight Principles, Zero Sideslip(엔진 부작동 비행 원리, 제로 사이드 슬립)