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飞机结冰引起的飞行动力学问题探讨 被引量:21

The Exploration of Flight Dynamics Problem on Aircraft Icing
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摘要 飞机在结冰后,飞行性能、稳定性、操纵性都受到不同程度的影响,对这些问题进行了阐述,并分析了其原因。为定性地说明问题,给出了一些算例和试飞数据。最后,概要性地分析了结冰后的飞行动力学问题,并展望了以后的研究方向。 The performance, stability and controllability of an aircraft were all affected after icing, in different degree. This paper expatiates on these effects and analyzes the causes of them. The simulation and flight test results were presented to illuminate the problem. At last, the flight dynamics problem on iced aircraft and future research were analyzed.
出处 《飞行力学》 CSCD 2004年第3期64-68,共5页 Flight Dynamics
关键词 飞机结冰 飞行力学 稳定性 操纵性 aircraft icing flight dynamics stability controllability
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参考文献4

  • 1Shim J,Chung J,Lee K D.A Computational Investigation of Ice Geometry Effects on Airfoil Performances[R].AIAA-2001-0540,2001.
  • 2Harold E Addy,Jr James J Chung.A Wind Tunnel Study of Icing Effects on a Natural Laminar Flow Airfoil[R].AIAA-2000-0095,2000.
  • 3Bragg M B,Hutchison T,Merret J,et al.Effects of Ice Accretion on Aircraft Flight Dynamics[R].AIAA Paper No.2000-0360,2000.
  • 4Pokhariyal D,Bragg M B,Hutchison T,et al.Aircraft Flight Dynamics with Simulated Ice Accretion[R].AIAA-2001-0541,2001.

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