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本文根据美国《军用规范——有人驾驶飞机的飞行品质》[MIL-F-8785B]和苏联《飞机民用适航性标准》等规范要求,对运八飞机非对称动力情况下的飞行性能和飞行品质,在理论计算和飞行试验方面进行了讨论。并通过分析比较表明,理论与实际的一致性。同时提出了各种因素对非对称动力情况下的飞行性能和飞行品质的影响,并提出了非对称动力情况下的试飞方法.
Based on the requirements of the US “Military Specifications - Manned Flying Quality” [MIL-F-8785B] and the Soviet “Aircraft Civil Airworthiness Standards” and other specifications, this paper analyzes the flight performance and flight performance under the asymmetrical power Quality is discussed in theoretical calculations and flight tests. And through analysis and comparison shows that the theory and the actual consistency. At the same time, the influences of various factors on flight performance and flight quality under asymmetric motive force are put forward, and the flight test method under asymmetrical power condition is proposed.