Aeromechanic aspects in the design of the EC135

Konstantin Kampa; Bernhard Enenkl; Gunther Polz

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Aeromechanic aspects in the design of the EC135

机译：EC135设计中的空气力学方面

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This paper highlights the design work for optimized dynamics, aerodynamics, flying and handling qualities taking into account the experiences gained during the development of the EC135. First a brief description of the development schedule and heli- copter is given. then follows a discussion of interesting topics like rotor dynamics, vibration, rotor/airframe aerodynamics, sta- bility and control. For each problem area, significant parameters are discussed and tendencies are shown.

机译：本文重点介绍了优化动力，空气动力学，飞行和操纵质量的设计工作，同时考虑了EC135开发过程中获得的经验。首先，简要介绍了开发时间表和直升机。然后讨论有趣的话题，例如旋翼动力学，振动，旋翼/机身空气动力学，稳定性和控制。对于每个问题区域，讨论了重要的参数并显示了趋势。

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来源
《Journal of the American Helicopter Society》 |1999年第2期|p.83-93|共11页
作者
Konstantin Kampa; Bernhard Enenkl; Gunther Polz;
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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
原文格式 PDF
正文语种 eng
中图分类航空;
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Aeromechanic aspects in the design of the EC135

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