Research on effect airwake acts on glide performance of carrier-based aircraft

Yu Yongtao, Zhang Zhi
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引用次数: 2

Abstract

The kinematic model of carrier-based aircraft was established. The airwake model described in USA military standard was introduced and analyzed. A landing simulation system was build based on the kinematic model of aircraft and airwake model. Numerical simulation was carried out to research the effect that airwake acted on the flight performance of carrier-base aircraft. Simulation results show that the gliding track of aircraft affected by airwake is lower than reference gliding track, which reduces the landing safety. The random component and free-air turbulence component of airwake own the dominate part of effect, the steady component makes contribution too, the periodic component acts little effect on aircraft. Airwake affects flight performance of aircraft by putting effect on the aerodynamic force of aircraft but not aero dynamical moment.
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尾流对舰载机滑翔性能影响的研究
建立了舰载机的运动学模型。介绍并分析了美国军用标准中描述的气流模型。建立了基于飞行器运动学模型和尾流模型的着陆仿真系统。通过数值模拟研究了尾流对舰载机飞行性能的影响。仿真结果表明,受尾流影响的飞机滑行轨迹低于参考轨迹,降低了着陆安全性。尾流的随机分量和自由空气湍流分量对飞机的影响占主导地位,稳定分量也有贡献,周期分量对飞机的影响较小。尾流通过影响飞机的气动力而不是气动力矩来影响飞机的飞行性能。
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