樂(lè)嘉陵院士研究論文選集

目錄
序言
高超聲速非平衡流動(dòng)研究
高溫空氣總輻射強(qiáng)度的測(cè)定 (樂(lè)嘉陵) 3
Studies of nonequilibrium effects in nozzle flow under high reservoir conditions (Le Jialing，Dong Weizhong) 14
2H2+O2爆轟波后壁面熱交換測(cè)量 (樂(lè)嘉陵，杜錫鑫) 20
駐點(diǎn)壁面催化速率常數(shù)確定的研究 (董維中，樂(lè)嘉陵，劉偉雄) 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
高超聲速圓球模型飛行流場(chǎng)的數(shù)值模擬和實(shí)驗(yàn)驗(yàn)證 (柳軍，樂(lè)嘉陵，楊輝) 43
基于CFD的電磁散射數(shù)值模擬 (許勇，樂(lè)嘉陵) 51
強(qiáng)激波陣面的非平衡特性研究 (樂(lè)嘉陵，張若凌，王蘇，崔季平) 56
激波與流動(dòng)顯示研究
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
彩色計(jì)算干涉技術(shù)及應(yīng)用 (吳穎川，樂(lè)嘉陵，賀安之) 94
Some research in application of holographic interferometry and computational flow imaging JiaLing Le，Yingchuan Wu，Hongli Ni，Hui Yang，Huiling Wu) 102
激波繞楔形物體的流場(chǎng)分析 (王惠玲，樂(lè)嘉陵，吳穎川) 110
雙時(shí)間步方法的應(yīng)用分析 (趙慧勇，樂(lè)嘉陵) 116
高超聲速技術(shù)研究
高超聲速飛行器的碳?xì)淙剂想p模態(tài)超燃沖壓方案研究 (樂(lè)嘉陵，劉陵) 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
脈沖燃燒風(fēng)洞及其在火箭和超燃發(fā)動(dòng)機(jī)研究中的應(yīng)用 (樂(lè)嘉陵，劉偉雄，賀偉，譚宇，白菡塵) 144
超燃沖壓發(fā)動(dòng)機(jī)再生冷卻熱結(jié)構(gòu)設(shè)計(jì)的計(jì)算工具 (蔣勁，張若凌，樂(lè)嘉陵) 154
甲烷點(diǎn)火燃燒的簡(jiǎn)化化學(xué)反應(yīng)動(dòng)力學(xué)模型研究 (肖保國(guó)，錢(qián)煒祺，楊順華，樂(lè)嘉陵) 161
一體化高超聲速飛行器氣動(dòng)-推進(jìn)性能評(píng)估 (賀元元，倪鴻禮，樂(lè)嘉陵) 166
超聲速氣流中液體燃料霧化數(shù)值模擬 (楊順華，樂(lè)嘉陵) 171
火焰面模型在超燃沖壓發(fā)動(dòng)機(jī)數(shù)值模擬中的應(yīng)用 (邢建文，樂(lè)嘉陵) 175
煤油超燃沖壓發(fā)動(dòng)機(jī)三維大規(guī)模并行數(shù)值模擬 (楊順華，樂(lè)嘉陵，趙慧勇，鄭中華) 181
Experimental and numerical investigation of air vitiation effects on scramjet test performance (JiaLing Le，Weixiong Liu，Wenyan Song，Jianwen Xing，Yang Yang) 188
超聲速化學(xué)反應(yīng)流動(dòng)的LU-SGS偽時(shí)間迭代空間推進(jìn)求解 (賀旭照，樂(lè)嘉陵，宋文艷) 200
超聲速冷態(tài)流場(chǎng)液體射流霧化實(shí)驗(yàn)研究 (陳亮，樂(lè)嘉陵，宋文艷，楊順華，曹娜) 206
Numerical investigations of unsteady spray combustion in a liquid kerosene fueled scramjet (Jialing Le，Shunhua Yang，Xiyao Wang) 213
超燃沖壓發(fā)動(dòng)機(jī)帶凹槽的燃燒室流場(chǎng)振蕩研究 (王西耀，楊順華，樂(lè)嘉陵) 222
馬赫數(shù)為4的超燃發(fā)動(dòng)機(jī)碳?xì)淙剂宵c(diǎn)火試驗(yàn) (張彎洲，樂(lè)嘉陵，楊順華，程文明，鄧維鑫，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
超臨界壓力下正十烷流動(dòng)傳熱的數(shù)值模擬 (趙國(guó)柱，宋文艷，張若凌，樂(lè)嘉陵) 244
吸氣式高超聲速飛行器機(jī)體推進(jìn)一體化技術(shù)研究進(jìn)展 (吳穎川，賀元元，賀偉，樂(lè)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
強(qiáng)制轉(zhuǎn)捩對(duì)高超聲速進(jìn)氣道性能影響 (易淼榮，趙慧勇，樂(lè)嘉陵) 280
亞聲速橫向氣流中液體射流破碎過(guò)程的直接模擬 (劉日超，樂(lè)嘉陵，楊順華，鄭忠華，宋文艷，黃淵) 288
電加熱圓管內(nèi)流動(dòng)的自然轉(zhuǎn)捩過(guò)程研究 (張若凌，樂(lè)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
徑向雙旋流燃燒室流場(chǎng)結(jié)構(gòu)大渦模擬研究 (周瑜，樂(lè)嘉陵，陳柳君，黃淵) 333
軸向三級(jí)旋流燃燒室流場(chǎng)結(jié)構(gòu)大渦模擬 (周瑜，樂(lè)嘉陵，陳柳君，黃淵) 342
Design and analysis osculating general curved cone waverider (Xuzhao He，Jialing Le，Si Qin) 351
附錄 樂(lè)嘉陵院士發(fā)表的論文 358