基于广义Burgers方程的超声速客机远场声爆高精度预测方法

乔建领; 韩忠华; 丁玉临; 池江波; 孟冠宇; 宋笔锋; 宋文萍

doi:10.7638/kqdlxxb-2018.0267

欢迎来到能源电力期刊网！

English Version 期刊登录

您当前的位置：

首页 >

文章列表页 >

基于广义Burgers方程的超声速客机远场声爆高精度预测方法

专栏——声爆研究 | 更新时间：2026-05-28

- 基于广义Burgers方程的超声速客机远场声爆高精度预测方法
- Sonic boom prediction method for supersonic transports based on augmented Burgers equation
- 空气动力学学报 2019年37卷第4期页码：663-674
- 作者机构：
  
  1. 西北工业大学航空学院超声速客机研究中心,西安,710072
  2. 西北工业大学航空学院气动与多学科优化设计研究所,西安,710072
- 作者简介：
  
  乔建领(1994-), 男, 山东菏泽人, 博士研究生, 研究方向:超声速客机声爆预测与低声爆优化设计.E-mail:qiaojianling@163.com
  韩忠华(1977-), 男, 四川资中人, 教授/博导, 研究方向:代理模型及代理优化理论和算法, 气动与多学科优化设计基础理论与算法, 翼型/机翼/飞行器气动设计, 超声速客机声爆预测与低声爆设计等.E-mail:hanzh@nwpu.edu.cn
- 基金信息：
  
  国家自然科学基金（11772261）;航空科学基金（2016ZA53011）;CFD前沿技术项目（2015-F-016）
- DOI：10.7638/kqdlxxb-2018.0267
  中图分类号： V211.3
- 纸质出版：2019
- 稿件说明：
移动端阅览
乔建领, 韩忠华, 丁玉临, 池江波, 孟冠宇, 宋笔锋, 宋文萍. 基于广义Burgers方程的超声速客机远场声爆高精度预测方法[J]. 空气动力学学报, 2019, 37(4): 663-674.

QIAO Jianling, HAN Zhonghua, DING Yulin, et al. Sonic boom prediction method for supersonic transports based on augmented Burgers equation[J]. 2019, 37(4): 663-674.
乔建领, 韩忠华, 丁玉临, 池江波, 孟冠宇, 宋笔锋, 宋文萍. 基于广义Burgers方程的超声速客机远场声爆高精度预测方法[J]. 空气动力学学报, 2019, 37(4): 663-674. DOI： 10.7638/kqdlxxb-2018.0267.

QIAO Jianling, HAN Zhonghua, DING Yulin, et al. Sonic boom prediction method for supersonic transports based on augmented Burgers equation[J]. 2019, 37(4): 663-674. DOI： 10.7638/kqdlxxb-2018.0267.

摘要

声爆高精度预测技术是新一代环保型超声速客机设计的核心关键技术之一。基于广义Burgers方程发展了可考虑"大气风"效应的远场高精度预测方法，开发了声爆预测程序"bBoom"，并研究了近场声爆信号提取位置和"大气风"对远场声爆计算结果的影响。首先，给出了广义Burgers方程和声爆传播射线的计算方法，重点讨论了方程中计算分子弛豫效应和热黏吸收效应的关键参数。其次，通过简单轴对称构型标模算例、NASA的C25D构型和洛马的LM1021构型等复杂超声速客机算例对所发展的方法进行了验证，表明本文发展的方法在预测远场声爆时具有较高可信度。最后，基于所发展的方法对比了由不同近场提取位置传播到地面的波形，研究了飞机向不同方向飞行时，"大气风"对地面声爆强度和地面影响域的影响。结果表明：对于类C25D标模构型，为了确保远场声爆预测结果具有较高精度，应取机身下方约3倍机身长度位置处的近场压强信号作为传播方程的输入；另外，"大气风"会影响地面声爆强度及地面影响域，在预测时有必要加以考虑。

Abstract

The high-fidelity sonic-boom prediction is crucial for the design of low-boom supersonic transport aircraft. In this article

a far-field sonic-boom prediction method solving the augmented Burgers equation is studied

and a prediction code called "bBoom" is developed. First

the numerical method for solving augmented Burgers equation and a ray tracing method in propagation are studied. Some significant parameters of molecular relaxation processes and thermoviscous absorption in the Burgers equation are presented. Second

some benchmark cases from the 2

AIAA Sonic Boom Prediction Workshop

including a simple axi-symmetric body

a NASA low-boom configuration

and LM1021 configuration

are employed to validate the code. The results show that the developed code is accurate and reliable for predicting the far-field waveforms. At last

far-field sonic boom waveforms propagated from different near-field pressure signals at different locations are compared

and the distinction of waveforms in different flight azimuthal angles with atmospheric winds is investigated. It is shown that

in order to improve the accuracy of predicting the sonic boom for configurations like a C25D model

the near-field signal should be extracted at a distance of three body lengths off the aircraft. It is also shown that atmospheric wind profiles have a significant impact on the sonic-boom waveform and sonic-boom carpet on the ground.

关键词

Keywords

references

PLOTKIN J K, MAGLIERI J D. Sonic boom research: history and future[R]. AIAA-2003-3575, 2003.

SAKATA K. Supersonic experimental airplane(NEXST) for next generation SST technology[R]. AIAA-2002-0527, 2002.

MORGENSTERN M J, STELMACK M, JHA D P. Advanced concept studies for supersonic commercial transports entering service in 2030-35 (N+3)[R]. AIAA-2010-5114, 2010.

WELGE H R, NELSON C, BONET J. Supersonic vehicle systems for the 2020 to 2035 timeframe[R]. AIAA-2010-4930, 2010.

WHITHAM G B. The flow pattern of a supersonic projectile[J]. Communications on Pure Applied Mathematics, 1952, 5(3):301-348.

WALKDEN F. The shock pattern of a wing-body combination, far from the flight path[J]. Aeronautical Quarterly, 1958, 9(2):164-194.

HAYES D W, HAEFELI C R, KULSRCD E H. Sonic boom propagation in a stratified atmosphere, with computer program[R]. NASA CR-1969-1299, 1969.

CARLSON HW. Simplified sonic-boom prediction[R]. NASA TP-1978-1122, 1978.

PLOTKINJ K. A rapid method for the computation of sonic booms[R]. AIAA-1993-4433, 1993.

YAMASHITA R, SUZUKI K. Full-field sonic boom simulation in real atmosphere[R]. AIAA-2014-2269, 2014.

YAMASHITA R, SUZUKI K. Rise time prediction of sonic boom by full-field simulation with thermal nonequilibrium[R]. AIAA-2015-2583, 2015.

YAMASHITA R, SUZUKI K. Full-field sonic boom simulation in stratified atmosphere[J]. AIAA Journal, 2016, 54(10):3223-3231.

THOMAS C L. Extrapolation of sonic boom pressure signatures by the waveform parameter method[R]. NASA TN D-1972-6832, 1972.

CLEVELAND R O. Propagation of sonic booms through a real, stratified atmosphere[D]. Austin: The University of Texas at Austin, 1995.

RALLABHANDI S K. Advanced sonic boom prediction using the augmented Burgers equation[J]. Journal of Aircraft, 2011, 48(4):1245-1253.

TAKENO J, MISAKA T, SHIMOYAMA K, et al. Analysis of sonic boom propagation based on the KZK equation[R]. AIAA-2015-0745, 2015.

PIERCE A D. Acoustics: an introductionto its physical principles and applications[M].Acoustical Soc. of America, 1981.

KANG J. Nonlinear acoustic propagation of shock waves through the atmosphere with molecular relaxation[D]. PA: The Pennsylvania State University, 1991.

ROBINSON L D.Sonic boom propagation through an inhomogeneous, windy atmosphere[D]. Austin: University of Texas at Austin, 1991.

ROBINSON L D. Anumerical model for sonic boom propagation through an inhomogeneous, windy atmoshpere[R]. NASA CP-1992-1372, 1992.

CLEVELAND R O. Effect of stratification and geometrical spreading on sonic boom rise time[R]. NASA N95-14880, 1995.

CLEVELAND R O. Propagation of sonic booms through a real, stratified atmosphere[D]. Austin: The University of Texas at Austin, 1995.

RALLABHANDI S K. Advanced sonic boom prediction using the augmented Burgers equation[J]. Journal of Aircraft, 2011, 48(4):1245-1253.

YAMAMOTO M, et al. Long-range sonic boom prediction considering atmospheric effects[C]//40th International Congress and Exposition on Noise Control Engineering 2011, INTER-NOISE, 2011.

YAMAMOTO M, et al. Numerical simulation for sonic boom propagation through an inhomogeneous atmosphere with winds[J]. AIP Conference Proceedings, 2012, 1474(1):339-342.

FENG X Q.The research of sonic boom prediction method and application in supersonic aircraft design[D]. Master Thesis, Xi'an: Northwestern Polytechnical University, 2012. (in Chinese)

FENG X Q. The research of low sonic boom mechanism and design method of supersonic aircraft[D]. Xi'an: Northwestern Polytechnical University, 2014. (in Chinese)

FENG X Q, LI Z K, SONG B F. Preliminary analysis on the sonic boom of supersonic aircraft[J]. Flight Dynamics, 2010, 28(6):21-23. (in Chinese)

FENG X Q, SONG B F, LI Z K. Research of low sonic boom quiet spike design method[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(5):1009-1017. (in Chinese)

FENG X Q, LI Z K, SONG B F. Research of low boom and low drag supersonic aircraft design[J]. Chinese Journal of Aeronautics, 2014, 27(3):531-541.

XU Y, SONG W Q. Near field sonic boom calculation on typical LSB configurations[J].Aeronautical Science Technology, 2016, 27(7):12-16. (in Chinese)

徐悦.超音速飞行器地面音爆强度预测方法对比研究[C]//全国气动声学学术会议, 2016.

WANG G, MA B P, LEI Z J, et al. Simulation and analysis for sonic boom on several benchmark cases[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1):164-176. (in Chinese)

MA B P, WANG G, LEI Z J, et al.Numerical investigation of influence of mesh property in nearfield sonic boom prediction[J]. Journal of Northwestern Polytechnical University, 2018, 36(5):865-874. (in Chinese)

霍满, 谭廉华, 林大楷, 等.声爆标模近场计算对远场预测影响研究[C]//首届空气动力学大会, 绵阳: 中国空气动力学会, CARS-04-2018-122, 2018.

钱战森, 刘忠臣, 冷岩, 等. OS-X0试验飞行器声爆特性测量与数值模拟分析[C]//首届空气动力学大会, 绵阳: 中国空气动力学会, CARS-04-2018-116, 2018.

ZHANG Y D, HUANG J T, GAO Z H. Far field simulation and applications of sonic boom based on augmented Burgers equation[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(7):122039. (in Chinese)

PIERCE D A. Acoustics-an introduction to its physical principles and applications[M]. New York:Acoustical Society of America, 1989, 587-588.

BASS E H, SUTHERLAND, C L, ZUCKERWAR J A, et al. Atmospheric absorption of sound:further developments[J]. Journal of the Acoustical Society of America, 1995, 97(1):680-683.

ONYEONWU R O. The effects of wind and temperature gradients on sonic boom corridors[R]. Univ. of Toronto Inst. for Aerospace Studies TN-168, 1971.

YAMAMOTO M, SAKIA T. A unified approach to an augmented Burgers equationfor propagation of sonic booms[J]. Acoustical Society of America, 2015, 137(4):1857-1866.

LEE Y-S. Numerical solution of KZK equation for pulsed finite amplitude sound beams in thermoviscous fluids[D]. Austin: University of Texas at Austin, 1993.

LEE Y-S, HAMILTON F M. Time-domain modeling of pulsed finite-amplitude sound beams[J]. Journal of the Acoustical Society of America, 1995, 97(2):906-917.

PARK M A, NEMEC M. Nearfield summary and statistical analysis of the second AIAA sonic boom prediction workshop[R].AIAA-2017-3256, 2017.

RALLABHANDI S K. Summary of propagation cases of the second AIAA sonic boom prediction workshop[R].AIAA-2017-3257, 2017.

PLOTKIN J K. State of the art of sonic boom modeling[J]. Journal of the Acoustical Society of America, 2002, 111(1):530-536.

SALAMONE J. Sonic boom simulation using conventional audio equipment[R].Baltimore, Maryland, NOISE-CON-2004, 2004.

ANDERSON G R, AFTOSMIS M J, NEMEC M. Cart3D simulations for the second AIAA sonic boom prediction workshop[J]. Journal of Aircraft, 2019, 56(3):896-911.

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

超声速飞行器声爆/气动力综合设计技术研究

新一代环保型超声速客机气动相关关键技术与研究进展

交错型CPR方法的保正实现策略及其对比研究

水滴撞击运动超疏水表面特性及其调控

离心通风机降噪研究进展