| Citation: | ZHU Wei, HUA Zhengxu, WANG Xiao. Variable angle of attack start experiment of 2D curved compression inlet[J]. Journal of Aerospace Power, 2020, 35(5): 992-999. doi: 10.13224/j.cnki.jasp.2020.05.011
|
| [1] |
EDWARDS C L W,SMAll W J,WEIDNER J P,et al.Studies of scramjet/airframe integration techniques for hypersonic aircraft［R］.AIAA 75-58,1975.
|
| [2] |
张堃元.基于弯曲激波压缩系统的高超声速进气道反设计研究进展［J］.航空学报,2015,36(1):274-288. ZHANG Kunyuan.Research progress on hypersonic inlet reverse design based on curved shock compression system［J］.Acta Aeronautica et Astronautica Sinica,2015,36(1):274-288.(in Chinese)
|
| [3] |
南向军,张堃元,金志光,等.压升规律可控的高超声速内收缩进气道设计［J］.航空动力学报,2011,26(3):518-523. NAN Xiangjun,ZHANG Kunyuan,JIN Zhiguang,et al.Investigation on hypersonic inward turning inlets with controlled pressure gradient［J］.Journal of Aerospace Power,2011,26(3):518-523.(in Chinese)
|
| [4] |
WANG Lei,ZHANG Kunyuan,NAN Xiangjun,et al.Optimization and experimental investigation of 2-D hypersonic curved shock［R］.AIAA-2012-5959,2012.
|
| [5] |
王磊,张堃元,向有志,等.高超声速二元弯曲激波压缩面反设计方法的参数化研究［J］.南京航空航天大学学报,2013,45(4):441-446. WANG Lei,ZHANG Kunyuan,XIANG Youzhi,et al.2-D hypersonic curved shock compression surface［J］.Journal of Nanjing University of Aeronautics and Astronautics,2013,45(4):441-446.(in Chinese)
|
| [6] |
李永洲,张堃元,南向军.基于马赫数分布规律可控概念的高超声速内收缩进气道设计［J］.航空动力学报,2012,27(11):2484-2491. LI Yongzhou,ZHANG Kunyuan,NAN Xiangjun.Design of hypersonic inward turning inlets base on concept of controllable Mach number distribution［J］.Journal of Aerospace Power,2012,27(11):2484-2491.(in Chinese)
|
| [7] |
朱伟.基于马赫数分布规律的高超矩形转圆内转式进气道设计研究［D］.南京:南京航空航天大学,2012. ZHU Wei.Investigation on hypersonic rectangular to circle shape transition inward turning inlets with controlled Mach number distributions［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2012.(in Chinese)
|
| [8] |
朱伟,张堃元,南向军.壁面马赫数分布规律可控的新型内收缩基准流场设计方法［J］.推进技术,2013,34(4):433-438. ZHU Wei,ZHANG Kunyuan,NAN Xiangjun.Investigation on basic flowfield with controlled Mach number gradient for hypersonic inward turning inlets［J］.Journal of Propulsion Technology,2013,34(4):433-438.(in Chinese)
|
| [9] |
张林,张堃元,王磊,等.基于壁面马赫数梯度的高超声速弯曲激波二维进气道数值研究［J］.航空动力学报,2013,28(4):752-758. ZHANG Lin,ZHANG Kunyuan,WANG Lei,et al.Computational investigation of hypersonic curved shock two-dimensional inlet with compression surface constant Mach number gradient［J］.Journal of Aerospace Power,2013,28(4):752-758.(in Chinese)
|
| [10] |
周硕,张堃元,王磊.高超压缩面分段反设计研究［R］.北京:高超声速专题研讨会暨第5届全国高超声速科学技术会,2012.
|
| [11] |
VAN WIE D,KWOK F T,WALSH R F.Starting characteristics of supersonic inlet［R］.AIAA 96-2914,1996.
|
| [12] |
王翼.高超声速进气道启动问题研究［D］.长沙:国防科技大学,2008. WANG Yi.Investigation on the starting characteristics of hypersonic inlet［D］.Changsha:National University of Defense Technology,2008.(in Chinese)
|
| [13] |
余安远,乐嘉陵.高超声速进气道起动问题的二维数值模拟初探［R］.南京:高超声速进气道技术交流(研讨)会,2005.
|
| [14] |
李祝飞,高文智,杨基明.一种二元进气道起动特性的数值与实验考察［J］.推进技术,2016,37(7):1224-1232. LI Zhufei,GAO Wenzhi,YANG Jiming.Numerical and experimental investigation for starting characteristics of a two-dimensional inlet［J］.Journal of Propulsion Technology,2016,37(7):1224-1232.(in Chinese)
|
| [15] |
刘雄,王翼,梁剑寒.二维高超声速进气道加速启动过程数值研究［J］.推进技术,2015,36(3):328-335. LIU Xiong,WANG Yi,LIANG Jianhan.Numerical research on accelerating starting of 2-dimensional hypersonic inlet［J］.Journal of Propulsion Technology,2015,36(3):328-335.(in Chinese)
|
| [16] |
游进,夏智勋,王登攀,等.高超声速进气道再起动特性及其影响因素数值模拟［J］.固体火箭技术,2011,34(2):161-166. YOU Jin,XIA Zhixun,WANG Dengpan,et al.Numerical study on influencing factors of restarting characteristics for a hypersonic inlet［J］.Journal of Solid Rocket Technology,2011,34(2):161-166.(in Chinese)
|
| [17] |
岳连捷,刘红,徐骁,等.激波风洞进气道自起动实验方法［C］∥第9届全国实验流体力学学术会议论文集.杭州:中国力学学会,2013:29-35.
|
| [18] |
WANG Yi,WANG Zhenguo,LIANG Jianhan,et al.Investigation on hypersonic inlet starting process in continuous freejet wind tunnel［J］.Journal of Propulsion and Power,2014,30(6):1721-1726.
|
| [19] |
GRAINGER A L,BOYCE R R,TIRTEY S C,et al.The unsteady flow physics of hypersonic inlet starting processes［R］.AIAA-2012-5937,2012.
|
| [20] |
谢文忠,葛严,赵昊,等.一种高超声速进气道加速自起动的实验方法［J］.航空动力学报,2018,33(6):1475-1483. XIE Wenzhong,GE Yan,ZHAO Hao,et al.A test method for accelerating self-start of hypersonic inlets［J］.Journal of Aerospace Power,2018,33(6):1475-1483.(in Chinese)
|
| [21] |
徐尚成,王翼,苏丹,等.迎角变化引起的高超声速进气道起动迟滞现象试验研究［J］.实验流体力学,2019,33(3):76-82. XU Shangcheng,WANG Yi,SU Dan,et al.Experimental study on hysteresis phenomenon of hypersonic inlet caused by variation of angle of attack［J］.Journal of Experiments in Fluid Mechanics,2019,33(3):76-82.(in Chinese)
|
DownLoad: