本文所采用的确定飞机性能的方法,不是直接用极曲线和推力测量,而是充分利用能反映飞机性能的剩余推力。本文旨在通过各种机动飞行,荻得“最大”状态、“加力”状态、亚音速和跨音速典型的相似参数综合特性线,利用这些曲线可计算飞机大速度、稳定盘旋,跃升拉起和盘旋上升等一些典型性能。文中还探索了飞机加速和减速、爬高等动作对发动机状态的影响。 Instead of using polar curves and thrust measurements directly, the method used to determine aircraft performance in this paper takes full advantage of the remaining thrust that reflects aircraft performance. The purpose of this paper is to calculate the large speed, steady circling and leaping up of the aircraft through various typical characteristics of maneuver flight, “maximum” state, “afterburner” state, subsonic and transonic typical similar parameters And spiraling up some of the typical performance. The article also explores the aircraft acceleration and deceleration, climbing and other actions on the state of the engine.