F-35平尾喷流效应和机动性  

F-35 Jet Flow Effect and Maneuverability

作　　者：吴健[1] WU Jian(Northwestern Polytechnical University,Xi’an 710072,China)

机构地区：[1]西北工业大学,陕西西安710072

出　　处：《系统仿真技术》2024年第1期60-64,共5页System Simulation Technology

摘　　要：本研究主要探讨F-35的平尾喷流效应。根据公开数据,在不高估性能的前提下,建立F-35的动力学模型并进行仿真,将仿真结果与F-35的飞行测试记录进行比较,并且和其他高机动性机型进行比较。仿真结果表明,仿真与飞行测试记录吻合,喷流效应对F-35机动性有较为明显的提升。This paper is focused on the effect of F-35 horizontal jet.Based on the published data and without overestimating its performance,the F-35 of the dynamic model is established,and simulation is carried out.The simulation results are compared with its flight test data,and also with other highly maneuverable aircraft.It is showed that the simulation result is matched with the flight test data,and the jet effect is very helpful for improving the F-35 maneuverability.

关 键 词：F-35 苏-27 米格-29 苏-57 喷流效应 机动性 

分 类 号：V221.3[航空宇航科学与技术—飞行器设计]