超声速民机和降低音爆研究

doi:10.7527/S1000-6893.2014.0207

流体力学与飞行力学

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超声速民机和降低音爆研究

朱自强, 兰世隆

北京航空航天大学航空科学与工程学院, 北京 100191

收稿日期:2014-07-02 修回日期:2014-09-15 出版日期:2015-08-15 发布日期:2015-09-29
通讯作者: 朱自强男, 教授, 博士生导师。《航空学报》第六、七届主编, 第八届编委。主要研究方向:计算流体力学, 飞行器气动设计。Tel: 010-82314186 E-mail: zhuzq@buaa.edu.cn E-mail:zhuzq@buaa.edu.cn
作者简介:兰世隆男, 博士, 副教授。主要研究方向:计算流体力学, 仿生流体力学, 气动噪声。Tel: 010-82317506 E-mail: lanshilong@126.com

Study of supersonic commercial transport and reduction of sonic boom

ZHU Ziqiang, LAN Shilong

School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China

Received:2014-07-02 Revised:2014-09-15 Online:2015-08-15 Published:2015-09-29
Contact: 10.7527/S1000-6893.2014.0207 E-mail:zhuzq@buaa.edu.cn

摘要/Abstract

摘要：

本文在简述超声速民机(SCT)的发展历史后,介绍了正在研制的几种超声速公务机的特点和未来(2020-2035年)超声速小型民机概念研究的进展及其可能的外形特点。由于降低音爆是当前发展SCT的首要任务之一,因此重点讨论了当前降低音爆的优化设计方法,主要包括:基于线性理论的设计方法;基于Euler解算器(Cart3D)和伴随方法的低音爆反设计方法;广义Burgers方程描述波的传播及其求解方法;以音爆造成地面噪声最小为目标,直接耦合音爆传播和CFD流场解的优化设计方法;可用于概念设计的多重优化设计方法等。

关键词: 超声速民机, 音爆, 降低音爆, 优化设计, CFD

Abstract:

Following a brief introduction of the development history of the supersonic commercial transport (SCT), the characteristics of several developing supersonic business jets are given. The conceptual design research of the small supersonic commercial transport being served during the period 2020-2035 and their possible configurations and features are described, too. Due to sonic boom reduction being one of the main tasks for developing SCT, some optimal design methods for reducing sonic boom are discussed in detail in the present paper, which are the design method based on linearized theory, sonic boom mitigation method using inverse design of coupling Euler solver (Cart3D) and adjoint method, the approach of advanced sonic boom prediction using augmented Burgers equation, the formulation that boom propagation and CFD are formally coupled for the purpose of obtaining gradients of a ground-based objective with respect to the aircraft shape design variables, as well as the optimization and adjoint-based CFD for the conceptual design of low sonic boom aircraft.

Key words: supersonic commercial transport, sonic boom, reduction of sonic boom, optimal design, CFD

中图分类号:

V211.3

朱自强, 兰世隆. 超声速民机和降低音爆研究[J]. 航空学报, 2015, 36(8): 2507-2528.

ZHU Ziqiang, LAN Shilong. Study of supersonic commercial transport and reduction of sonic boom[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(8): 2507-2528.

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超声速民机和降低音爆研究

Study of supersonic commercial transport and reduction of sonic boom

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