乐嘉陵院士研究论文选集

目录
序言
高超声速非平衡流动研究
高温空气总辐射强度的测定 (乐嘉陵) 3
Studies of nonequilibrium effects in nozzle flow under high reservoir conditions (Le Jialing，Dong Weizhong) 14
2H2+O2爆轰波后壁面热交换测量 (乐嘉陵，杜锡鑫) 20
驻点壁面催化速率常数确定的研究 (董维中，乐嘉陵，刘伟雄) 24
The calculations of aerodynamic heating and viscous friction forces on the surface of hypersonic flight vehicle (Le Jialing，VL Ganimedov，M I Muchnaja，V N Vetlutsky) 30
高超声速圆球模型飞行流场的数值模拟和实验验证 (柳军，乐嘉陵，杨辉) 43
基于CFD的电磁散射数值模拟 (许勇，乐嘉陵) 51
强激波阵面的非平衡特性研究 (乐嘉陵，张若凌，王苏，崔季平) 56
激波与流动显示研究
Mach reflection flow at hypersonic speeds (Le Jialing，Ni Hongli，Hu Guangchu 67
Study of the propagation of shock waves over bodies with holographic interferometry (Le Jialing，Ye Xichao，Wu Xingyan，Yang Hui) 73
Numerical simulation of shock (blast) wave interaction with bodies (Le Jia-ling，Ni Hong-li) 79
Research on blast wave interaction with body traveling supersonically (Ni Hong-li，Le Jia-ling) 88
彩色计算干涉技术及应用 (吴颖川，乐嘉陵，贺安之) 94
Some research in application of holographic interferometry and computational flow imaging JiaLing Le，Yingchuan Wu，Hongli Ni，Hui Yang，Huiling Wu) 102
激波绕楔形物体的流场分析 (王惠玲，乐嘉陵，吴颖川) 110
双时间步方法的应用分析 (赵慧勇，乐嘉陵) 116
高超声速技术研究
高超声速飞行器的碳氢燃料双模态超燃冲压方案研究 (乐嘉陵，刘陵) 125
Preliminary investigation of full model of two-mode scramjet (J.L. Le，Z.C. Zhang，H.C. Bai，M.A. Goldfeld，R.V. Nestoulia，A.V. Starov) 138
脉冲燃烧风洞及其在火箭和超燃发动机研究中的应用 (乐嘉陵，刘伟雄，贺伟，谭宇，白菡尘) 144
超燃冲压发动机再生冷却热结构设计的计算工具 (蒋劲，张若凌，乐嘉陵) 154
甲烷点火燃烧的简化化学反应动力学模型研究 (肖保国，钱炜祺，杨顺华，乐嘉陵) 161
一体化高超声速飞行器气动-推进性能评估 (贺元元，倪鸿礼，乐嘉陵) 166
超声速气流中液体燃料雾化数值模拟 (杨顺华，乐嘉陵) 171
火焰面模型在超燃冲压发动机数值模拟中的应用 (邢建文，乐嘉陵) 175
煤油超燃冲压发动机三维大规模并行数值模拟 (杨顺华，乐嘉陵，赵慧勇，郑中华) 181
Experimental and numerical investigation of air vitiation effects on scramjet test performance (JiaLing Le，Weixiong Liu，Wenyan Song，Jianwen Xing，Yang Yang) 188
超声速化学反应流动的LU-SGS伪时间迭代空间推进求解 (贺旭照，乐嘉陵，宋文艳) 200
超声速冷态流场液体射流雾化实验研究 (陈亮，乐嘉陵，宋文艳，杨顺华，曹娜) 206
Numerical investigations of unsteady spray combustion in a liquid kerosene fueled scramjet (Jialing Le，Shunhua Yang，Xiyao Wang) 213
超燃冲压发动机带凹槽的燃烧室流场振荡研究 (王西耀，杨顺华，乐嘉陵) 222
马赫数为4的超燃发动机碳氢燃料点火试验 (张弯洲，乐嘉陵，杨顺华，程文明，邓维鑫，周化波) 229
Experimental investigation on heat transfer correlations of n-decane under supercritical pressure (Zhang，R.L. Zhang，S.D. Xiao，J. Jiang，J.L. Le) 236
超临界压力下正十烷流动传热的数值模拟 (赵国柱，宋文艳，张若凌，乐嘉陵) 244
吸气式高超声速飞行器机体推进一体化技术研究进展 (吴颖川，贺元元，贺伟，乐嘉陵) 251
Investigation of combustion and flame stabilization modes in a hydrogen fueled scramjet combustor (Tian Ye，.Yang Shunhua，Le Jialing，Su Tie，Yue Maoxiong，Zhong Fuyu，Tian Xiaoqiang) 267
强制转捩对高超声速进气道性能影响 (易淼荣，赵慧勇，乐嘉陵) 280
亚声速横向气流中液体射流破碎过程的直接模拟 (刘日超，乐嘉陵，杨顺华，郑忠华，宋文艳，黄渊) 288
电加热圆管内流动的自然转捩过程研究 (张若凌，乐嘉陵) 295
Experimental and simulation study of aeroengine combustor based on CARS technology and UFPV approach (Xiong Moyou，Le Jialing，Huang Yuan，Song Wenyan，Yang shunhua，Zheng Zhonghua) 305
Investigation of combustion process of a kerosene fueled combustor with air throttling (Tian Ye，Yang Shunhua，Le Jialing，Zhong Fuyu，Tian Xiaoqiang) 314
Experimental research of air-throttling ignition for scramjet at Ma 6.5 (Weixin Deng，Jialing Le，Shunhua Yang，Wanzhou Zhang，Ye Tian) 326
径向双旋流燃烧室流场结构大涡模拟研究 (周瑜，乐嘉陵，陈柳君，黄渊) 333
轴向三级旋流燃烧室流场结构大涡模拟 (周瑜，乐嘉陵，陈柳君，黄渊) 342
Design and analysis osculating general curved cone waverider (Xuzhao He，Jialing Le，Si Qin) 351
附录 乐嘉陵院士发表的论文 358