航空学报 > 1996, Vol. 17 Issue (S1): 53-55

烟气流对飞机进场着陆影响的数值仿真研究

金长江, 洪冠新, 韩潮   

  1. 北京航空航天大学509教研室, 北京, 100083
  • 收稿日期:1996-01-25 修回日期:1996-04-25 出版日期:1996-11-25 发布日期:1996-11-25

NUMERICAL SIMULATION OF INFLUENCE OF HOT SMOKE STREAM ON AIRCRAFT′S APPROACH FLIGHT

Jin Changjiang, Hong Guanxin, Han Chao   

  1. Faculty 509,Beijing University of Aeronautics and Astronautics, Beijing,100083
  • Received:1996-01-25 Revised:1996-04-25 Online:1996-11-25 Published:1996-11-25

摘要: 飞机穿越高烟囱排放的高速热气流,尤其是在起飞和进场着陆阶段,烟气流场将影响飞机的航迹保持,造成颠簸,或影响乘座舒适性。用数值仿真方法论证飞机在正常飞行和非正常飞行、开环操纵和闭环操纵、有风和静风情况下,穿越烟气流场的运动特性。实践证明论证结论与飞行结果一致

关键词: 烟气流, 仿真, 进场

Abstract: Flight safety and travel comfort are affected while an aircraft penetrates the hot smoke stream from the high chimney of coal burning power plants.Open loop and close loop states for normal flight and normal weather, abnormal flight and tranquil wind for different airplanes are numerically simulated. In study of dynamic properties of aircraft influenced by the hot smoke stream,the feedback control laws of energy altitude and its rate are used. Actual sensations and judgments of pilots making a penetrating flight over a power plant are proved and reproduced by the results of numerical simulation.

Key words: smokest ream, simulation, approach

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