目次 |
综述 |
战斗机大迎角气动特性研究技术的发展与应用 ------------------------------------------------------------------------------------------------------------------------王海峰,展京霞,陈 科,陈 翔,陈梓钧 (1) |
研究论文 |
基于压缩感知的高频响流场重构方法及其应用 ------------------------------------------------------------------------------------------------------------------------陈子玉,周楷文,刘应征,温 新 (26) |
反射激波冲击单模界面的不稳定性实验研究 ------------------------------------------------------------------------------------------------------------------------王宏辉,丁举春,司 廷,罗喜胜 (33) |
绕弹性水翼空化流激振动特性实验研究 ------------------------------------------------------------------------------------------------------------------------刘韵晴,郭一梦,黄 彪,吴 钦,王国玉 (41) |
湍流边界层大尺度相干运动的阵列 TRPIV 测量 ------------------------------------------------------------------------------------------------------------------------王 轩,范子椰,唐湛棋,姜 楠 (49) |
叶顶间隙流动中的涡结构实验研究 ------------------------------------------------------------------------------------------------------------------------刘玉文,徐良浩,张国平,刘建华,彭晓星 (57) |
专栏——内外流一体化技术 |
展向压力分布可控的前体/压缩面气动设计方法及其流动特性 ------------------------------------------------------------------------------------------------------------------------蔡 佳,黄河峡,唐学斌,谭慧俊,李 超,吕靖昊 (66) |
最小波阻锥导乘波体和三维内转式进气道一体化设计 ------------------------------------------------------------------------------------------------------------------------贺旭照,卫 锋,刘福军,陈圣兵 (77) |
内流壁温效应对高速飞行器气动特性的影响 ------------------------------------------------------------------------------------------------------------------------武利龙,罗金玲,李 超,肖志祥,操小龙 (84) |
二元外压式超声速进气道起飞过程的进发匹配特性 ------------------------------------------------------------------------------------------------------------------------高为民,田方超,杨瀚超 (92) |
高速飞行器的连续旋转爆震推进技术 ------------------------------------------------------------------------------------------------------------------------师迎晨,张任帅,计自飞,王 兵 (101) |
全流面乘波前体进气道设计方法 ------------------------------------------------------------------------------------------------------------------------吴颖川,贺元元,卫 锋,余安远 (114) |
基于微型叶片式涡流发生器的前体压缩面低能流掺混机理 ------------------------------------------------------------------------------------------------------------------------李 超,黄河峡,罗金玲,唐学斌,蔡 佳,谭慧俊 (119) |
轴对称内锥流动中马赫盘的形成与演化 ------------------------------------------------------------------------------------------------------------------------姬隽泽,李祝飞,司东现,张 涛,施崇广,尤延铖,杨基明 (129) |
激波风洞超燃冲压发动机推阻测量技术 ------------------------------------------------------------------------------------------------------------------------陈勇富,卢洪波,文 帅,陈 星,孙日明 (141) |
专栏——吸气式组合动力 |
可重复使用宽域高速飞行器低速段动力方案分析与选型 ------------------------------------------------------------------------------------------------------------------------陈操斌,牛 军 (150) |
马赫数 0 至 8 范围 RBCC 发动机特性 ------------------------------------------------------------------------------------------------------------------------刘 昊 (165) |
空气涡轮火箭发动机热力过程及工作特性 ------------------------------------------------------------------------------------------------------------------------南向谊,刘 轶,马 元,杨顺华,马继承 (181) |
预冷型组合循环发动机技术 ------------------------------------------------------------------------------------------------------------------------罗佳茂,杨顺华,母忠强,张弯洲,游 进 (190) |
高超声速发动机碳氢燃料预冷器换热特性 ------------------------------------------------------------------------------------------------------------------------刘银龙,徐国强,付衍琛,汤龙生,闻 洁,王 宇,周建兴 (208) |
XTER 内收缩组合进气道设计理念及气动特性 ------------------------------------------------------------------------------------------------------------------------蔡泽君,胡占仓,余联郴,洪唐宝,朱呈祥,尤延铖 (218) |
本期责编:王 颖 |
CONTENTS |
Review |
Development and application of aerodynamic research technologies for fighters at high angle of attack ------------------------------------------------------------------------------------------------------------------------WANG Haifeng, ZHAN Jingxia, CHEN Ke, CHEN Xiang, CHEN Zijun (1) |
Research Articles |
High-frequency flow field reconstruction method based on compressed sensing and its applications ------------------------------------------------------------------------------------------------------------------------CHEN Ziyu, ZHOU Kaiwen, LIU Yingzheng, WEN Xin (26) |
Richtmyer-Meshkov instability of a single-mode interface with reshock ------------------------------------------------------------------------------------------------------------------------WANG Honghui, DING Juchun, SI Ting, LUO Xisheng (33) |
Experimental investigations of cavitating flow induced vibration around a flexible hydrofoil ------------------------------------------------------------------------------------------------------------------------LIU Yunqing, GUO Yimeng, HUANG Biao, WU Qin, WANG Guoyu (41) |
Arrayed TRPIV measurement of large-scale coherent motions in turbulent boundary layer ------------------------------------------------------------------------------------------------------------------------WANG Xuan, FAN Ziye, TANG Zhanqi, JIANG Nan (49) |
Experiments of the vortical structure morphology in a tip clearance flow ------------------------------------------------------------------------------------------------------------------------LIU Yuwen, XU Lianghao, ZHANG Guoping, LIU Jianhua, PENG Xiaoxing (57) |
Column——Internal and External Flow Integration Technology |
Aerodynamic design method and flow features of forebody/compression surface with controlled lateral pressure
distribution ------------------------------------------------------------------------------------------------------------------------CAI Jia, HUANG Hexia, TANG Xuebin, TAN Huijun, LI Chao, LYU Jinghao (66) |
Integrated design of minimal wave drag cone-derived waveriders and three-dimensional inward turning inlets ------------------------------------------------------------------------------------------------------------------------HE Xuzhao, WEI Feng, LIU Fujun, CHEN Shengbing (77) |
Effect of inner flow wall temperature on the aerodynamic characteristics of high-speed vehicles ------------------------------------------------------------------------------------------------------------------------WU Lilong, LUO Jinling, LI Chao, XIAO Zhixiang, CAO Xiaolong (84) |
Study on the matching between a two-dimensional supersonic inlet and an aero-engine during take-off ------------------------------------------------------------------------------------------------------------------------GAO Weimin, TIAN Fangchao, YANG Hanchao (92) |
Rotating detonation propulsion technology for high-speed aircrafts ------------------------------------------------------------------------------------------------------------------------SHI Yingchen, ZHANG Renshuai, JI Zifei, WANG Bing (101) |
Design of continuous streamline tracing waverider forebody inlet ------------------------------------------------------------------------------------------------------------------------WU Yingchuan, HE Yuanyuan, WEI Feng, YU Anyuan (114) |
Mixing of low-momentum fluids over the forebody ramp based on micro-vane vortex generators ------------------------------------------------------------------------------------------------------------------------LI Chao, HUANG Hexia, LUO Jinling, TANG Xuebin, CAI Jia, TAN Huijun (119) |
Formation and evolution of Mach disk in axisymmetric internal conical flow ------------------------------------------------------------------------------------------------------------------------JI Junze, LI Zhufei, SI Dongxian, ZHANG Tao, SHI Chongguang, YOU Yancheng, YANG Jiming (129) |
Thrust/Drag measurement techniques of a free flight scramjet in a shock tunnel ------------------------------------------------------------------------------------------------------------------------CHEN Yongfu, LU Hongbo, WEN Shuai, CHEN Xing, SUN Riming (141) |
Column——Airbreathing Combined Propulsion |
Analysis and selection of engine schemes for reusable wide-range high-speed aircraft in the low-speed phase ------------------------------------------------------------------------------------------------------------------------CHEN Caobin, NIU Jun (150) |
Characteristic analysis of RBCC engine at Mach number 0 to 8 ------------------------------------------------------------------------------------------------------------------------ LIU Hao (165) |
Thermodynamic process and operating characteristics of air turbo rocket engine ------------------------------------------------------------------------------------------------------------------------NAN Xiangyi, LIU Yi, MA Yuan, YANG Shunhua, MA Jicheng (181) |
Technology analysis of pre-cooled combined-cycle engine ------------------------------------------------------------------------------------------------------------------------LUO Jiamao, YANG Shunhua, MU Zhongqiang, ZHANG Wanzhou, YOU Jin (190) |
Heat transfer characteristics of a hydrocarbon fuel precooler for hypersonic engines ------------------------------------------------------------------------------------------------------------------------LIU Yinlong, XU Guoqiang, FU Yanchen, TANG Longsheng, WEN Jie, WANG Yu, ZHOU Jianxing (208) |
Design concept and aerodynamic characteristics of XTER TBCC inlet ------------------------------------------------------------------------------------------------------------------------CAI Zejun, HU Zhancang, YU Lianchen, HONG Tangbao, ZHU Chengxiang, YOU Yancheng (218) |