无尾飞翼布局特殊舵面建模与气动弹性研究

张礼; 王正平; 高正红

doi:10.13433/j.cnki.1003-8728.2014.1028

无尾飞翼布局特殊舵面建模与气动弹性研究

doi: 10.13433/j.cnki.1003-8728.2014.1028

1.
西北工业大学航空学院, 西安 710072

详细信息

作者简介:
张礼(1982-)，博士研究生，研究方向为飞行器总体设计，taohailantian@126.com;王正平(联系人)，教授，ad502@nwpu.edu.cn

张礼(1982-)，博士研究生，研究方向为飞行器总体设计，taohailantian@126.com;王正平(联系人)，教授，ad502@nwpu.edu.cn

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出版历程
- 收稿日期: 2013-03-23

Study on the Modeling and Aeroelasticity for the Special Rudders of a Tailless Flying Wing Configuration

1.
School of Aeronautics, Northwest Polytechnical University, Xi'an 710072

摘要

摘要: 以多舵面组合下的无尾飞翼布局飞机为基础,建立全机的结构有限元模型和气动面模型。针对其双舵面的特点,进行气动与结构修正,从而比较真实的反映双舵面飞翼布局的气弹特性,提出了一种实用的建模和计算方法。
- 无尾飞翼布局 /
- 双舵面 /
- 气动弹性 /
- 气动力修正 /
- 操纵效率
Abstract: Based on one flying wing with multi-control surface and split rudder, the structural finite element modeland aerodynamic model were built.According to the characteristics of multi-control surfaces and split rudders themodification for aerodynamic model and structural model wereconducted, so the aeroelastic characteristics of theflying wing with split rudders are reasonable.The proposed modeling andcomputation method is practical.
- aerodynamic configurations /
- aerodynamics modification /
- aeroelasticity /
- ailerons /
- calculations

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参考文献(11)

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