飞行器动态稳定性参数计算方法研究进展

doi:10.7527/S1000-6893.2016.0098

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飞行器动态稳定性参数计算方法研究进展

刘绪, 刘伟, 柴振霞, 杨小亮

国防科学技术大学航天科学与工程学院, 长沙 410073

收稿日期:2016-01-11 修回日期:2016-03-23 出版日期:2016-08-15 发布日期:2016-03-28
通讯作者: 刘伟,Tel.:0731-84573137。E-mail:fishfather6525@sina.com E-mail:fishfather6525@sina.com
作者简介:刘绪,男,博士研究生。主要研究方向:高超声速空气动力学。Tel.:0731-84574792。E-mail:liuxuqd@126.com;刘伟,男,博士,教授。主要研究方向:计算流体力学研究与应用。Tel.:0731-84573137。E-mail:fishfather6525@sina.com;柴振霞,女,博士研究生。主要研究方向:频域计算方法在非定常流动中的应用。Tel.:0731-84574792。E-mail:chaizhenxia@sina.cn;杨小亮,男,博士,讲师。主要研究方向:计算流体力学研究与应用。Tel.:0731-84574792。E-mail:yangxl_nudt@sina.com
基金资助:
国家自然科学基金（11172325，11502292）；国防科学技术大学预研项目（ZDYYJCYJ20140101）

Research progress of numerical method of dynamic stability derivatives of aircraft

LIU Xu, LIU Wei, CHAI Zhenxia, YANG Xiaoliang

College of Areospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

Received:2016-01-11 Revised:2016-03-23 Online:2016-08-15 Published:2016-03-28
Supported by:
National Natural Science Foundation of China (11172325, 11502292);NUDT Advanced Project (ZDYYJCYJ20140101)

摘要/Abstract

摘要：

动态稳定性参数（简称动导数）是飞行器控制系统设计、飞行器动不稳定发生边界分析及相应动态稳定性判据研究的关键气动参数。在对飞行稳定性问题进行概述的基础上，介绍飞行器动态稳定性参数数值模拟的国内外研究进展。并按照理论方法、工程近似方法及计算流体力学（CFD）模拟方法的动导数发展方向对近年来主要的动导数计算方法进行了综述，评价了各种动导数预测方法的优缺点，指出了动导数数值模拟在理论基础、非定常气动力建模、预测方法精度和效率等方面存在的问题。最后对动导数数值模拟的发展趋势进行了展望。

关键词: 数值方法, 计算流体力学, 稳定性, 时域分析, 动导数

Abstract:

Dynamic stability derivatives (for short, dynamic derivatives) are key aerodynamic parameters for designing the control system, investigating the dynamic instability boundary and studying the dynamic stability criteria of aircraft. After a brief summary of flight stability, the research progress made in the numerical simulation of aircraft dynamic stability parameters is described. The main dynamic derivative calculation methods applied over the past few years are reviewed with respect to the theoretical method, engineering approximation and computational fluid dynamics (CFD) simulation. The merits of these dynamic derivative prediction methods are identified, and problems with numerical simulation of dynamic derivatives in terms of theoretical basis, unsteady aerodynamic modeling, the precision and efficiency of the prediction methods are pointed out. A mature, reliable prediction of dynamic stability characteristic enables us to evaluate and select different air design plans so as to minimize the aircraft design cost and mitigate risk exposure. Finally, the development trend of numerical simulation of dynamic derivatives is prospected.

Key words: numerical methods, computational fluid dynamics, stability, time domain analysis, dynamic derivatives

中图分类号:

V211.3

刘绪, 刘伟, 柴振霞, 杨小亮. 飞行器动态稳定性参数计算方法研究进展[J]. 航空学报, 2016, 37(8): 2348-2369.

LIU Xu, LIU Wei, CHAI Zhenxia, YANG Xiaoliang. Research progress of numerical method of dynamic stability derivatives of aircraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(8): 2348-2369.

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飞行器动态稳定性参数计算方法研究进展

Research progress of numerical method of dynamic stability derivatives of aircraft

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