论文:2020,Vol:38,Issue(2):231-237
引用本文:
余刚, 李栋, 张泽宇. 翼身融合布局起飞状态动力效应影响研究[J]. 西北工业大学学报
YU Gang, LI Dong, ZHANG Zeyu. Simulation on Powered Effects of BWB at Take-off Condition[J]. Northwestern polytechnical university

翼身融合布局起飞状态动力效应影响研究
余刚, 李栋, 张泽宇
西北工业大学 航空学院, 陕西 西安 710072
摘要:
以西北工业大学布局设计研究所设计的翼身融合布局民机构型BWB300为研究对象,对起飞状态下动力效应对其气动特性影响进行了数值模拟分析。首先,对设置进排气边界条件模拟发动机动力效应方法进行了验证。然后,通过对比分析分别安装通气短舱和动力短舱的BWB300起飞状态的数值模拟结果,研究了发动机动力效应对其气动特性的影响规律。研究结果表明:动力效应会增加构型的升阻力系数,改变其俯仰力矩系数,但不会改变气动曲线的变化趋势,通气和动力构型在最大升阻比和最大升力系数处的迎角相同。故在对BWB300飞发一体化设计分析中,使用动力短舱可获得更加精确的结果,但使用通气短舱,也可得出较为可靠的规律性结论。
关键词:    翼身融合布局    起飞状态    动力效应    气动特性    数值模拟   
Simulation on Powered Effects of BWB at Take-off Condition
YU Gang, LI Dong, ZHANG Zeyu
School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:
The influence of engine powered effects on aerodynamic characteristics of BWB300, which was designed by the Airplane Concept Design Institute of Northwestern Polytechnical University, at take-off condition was analyzed by using the numerical simulation method. Firstly, the method of using the inlet and exhaust boundary conditions to analyze the powered engine was validated. Then, the engine powered effects on BWB300 aerodynamic characteristics at take-off condition were researched with flow through nacelle and with powered nacelle. The results indicated that though the powered effect changing the value of aerodynamic forces, there was no change in the aerodynamic curve trend. It's recommended that the engine power effect should be considered in numerical simulation by using with powered nacelle to gain more accurate values of aerodynamic forces. Nevertheless, with flow nacelle also could be used to gain some regular results.
Key words:    BWB    take-off condition    powered effect    aerodynamic characteristics    numerical simulation   
收稿日期: 2019-06-05     修回日期:
DOI: 10.1051/jnwpu/20203820231
基金项目: 中央高校基本科研业务费专项资金(3102019JC009)资助
通讯作者:     Email:
作者简介: 余刚(1982-),西北工业大学博士研究生,主要从事气动布局设计及飞发一体化研究。
相关功能
PDF(1061KB) Free
打印本文
把本文推荐给朋友
作者相关文章
余刚  在本刊中的所有文章
李栋  在本刊中的所有文章
张泽宇  在本刊中的所有文章

参考文献:
[1] 张彬乾, 陈真利, 李杰. 亚音速大型民机气动布局发展趋势[C]//大型飞机关键技术高层论坛暨中国航空学会学术年会, 2007 ZHANG Binqian, CHEN Zhenli, LI Jie. Development Trend of Subsonic Large Civil Aircraft Aerodynamic Layout[C]//High-level Forum on Key Technologies for Large Aircraft and the Annual Academic Conference of the Chinese Society of Aeronautics and Astronautics, 2007(in Chinese)
[2] BRENNER M, TREPANIER J, TRIBES C, et al. Conceptual Design Framework for Blended Wing Body Airplane[C]//12th AIAA Aviation Technology, Integration, and Operations, 2012
[3] LIEBECK R, PAGE M, RAWDON B. Blended-Wing-Body Subsonic Commercial Transport[R]. AIAA-1998-0438
[4] OKONKWO P, SMITH H. Review of Evolving Trends in Blended Wing Body Aircraft Design[J]. Progress in Aerospace Sciences, 2016, 82:1-23
[5] RUDNIK R, ROSSOW C C, GEYR H F V. Numerical Simulation of Engine/Airframe Integration for High-Bypass Engines[J]. Aerospace Science & Technology, 2002, 6(1):31-42
[6] 李杰,鄂秦,李凤蔚. 翼吊式双发民机机体/动力装置一体化数值分析[J]. 力学学报,2000,32(2):233-238 LI Jie, E Qin, LI Fengwei. Numerical Simulation of Transonic Flow over Wing-Mounted Twin-Engine Transport Aircraft[J]. Acta Mechanica Sinica, 2000, 32(2):233-238(in Chinese)
[7] LONG K, SHEA P R, FLAMM J D, et al. Turbine Powered Simulator Calibration and Testing for Hybrid Wing Body Powered Airframe Integration[C]//AIAA Aerospace Sciences Meeting, 2016
[8] GARCIA J A, MELTON J, SCHUH M J, et al. NASA ERA Integrated CFD for Wind Tunnel Testing of Hybrid Wing-Body Configuration[C]//AIAA Aerospace Sciences Meeting, 2016
[9] SCHUH M J, GARCIA J A, CARTER M B, et al. NASA Environmentally Responsible Aviation Hybrid Wing Body Flow-Through Nacelle Wind Tunnel CFD[C]//AIAA Aerospace Sciences Meeting, 2016
[10] 谭兆光, 陈迎春, 李杰, 等. 机体/动力装置一体化分析中的动力影响效应数值模拟[J]. 航空动力学报, 2009, 24(8):1766-1772 TAN Zhaoguang, CHEN Yingchun, LI Jie, et al. Numerical Simulation Method for the Powered Effects in Airframe/Propulsion Integration Analysis[J]. Journal of Aerospace Power, 2009, 24(8):1766-1772(in Chinese)
[11] 郭少杰, 周培培, 王斌,等. 动力效应对民机起飞构型气动特性影响的数值研究[J]. 航空动力学报, 2016, 31(7):1638-1648 GUO Shanjie, ZHOU Peipei, WANG Bin, et al. Numercial Investigation for Influence of Powered Effect on Aerodynamic Characteristics of Civil Aircraft Take-off Configuration[J]. Journal of Aerospace Power, 2016, 31(7):1637-1648(in Chinese)
[12] HIROSE N, ASAI K, IKAWA K. Transonic 3-D Euler Analysis of Flows around Fan-Jet Engine and T. P. S. (Turbine Powered Simulator)[R]. NAL-TR-1045, 1989
[13] HIROSE N, ASAI K, IKAWA K, et al. 3-D Euler Flow Analysis of Fanjet Engine and Turbine Powered Simulator with Experimental Comparison in Transonic Speed[R]. AIAA-1989-1835