目錄
序言
高超聲速非平衡流動研究
高溫空氣總輻射強度的測定 (樂嘉陵) 3
Studies of nonequilibrium effects in nozzle flow under high reservoir conditions (Le Jialing，Dong Weizhong) 14
2H2 O2爆轟波後壁面熱交換測量 (樂嘉陵，杜錫鑫) 20
駐點壁面催化速率常數確定的研究 (董維中，樂嘉陵，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的數值模擬和實驗驗證 (柳軍，樂嘉陵，楊輝) 43
基於CFD的電磁散射數值模擬 (許勇，樂嘉陵) 51
強激波陣面的非平衡特性研究 (樂嘉陵，張若凌，王蘇，崔季平) 56
激波與流動顯示研究
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
彩色計算干涉技術及應用 (吳穎川，樂嘉陵，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分析 (王惠玲，樂嘉陵，吳穎川) 110
雙時間步方法的應用分析 (趙慧勇，樂嘉陵) 116
高超聲速技術研究
高超聲速飛行器的碳氫燃料雙模態超燃衝壓方案研究 (樂嘉陵，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
脈衝燃燒風洞及其在火箭和超燃發動機研究中的應用 (樂嘉陵，劉偉雄，賀偉，譚宇，白菡塵) 144
超燃衝壓發動機再生冷卻熱結構設計的計算工具 (蔣勁，張若凌，樂嘉陵) 154
甲烷點火燃燒的簡化化學反應動力學模型研究 (肖保國，錢煒祺，楊順華，樂嘉陵) 161
一體化高超聲速飛行器氣動-推進性，倪鴻禮，樂嘉陵) 166
超聲速氣流中液體燃料霧化數值模擬 (楊順華，樂嘉陵) 171
火焰面模型在超燃衝壓發動機數值模擬中的應用 (邢建文，樂嘉陵) 175
煤油超燃衝壓發動機三維大規模並行數值模擬 (楊順華，樂嘉陵，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
超聲速化學反應流動的LU-SGS偽時間迭代空間推進求解 (賀旭照，樂嘉陵，宋文艷) 200
超聲速冷態流場液體射流霧化實驗研究 (陳亮，樂嘉陵，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
超燃衝壓發動機帶凹槽的燃燒室流場振蕩研究 (王西耀，楊順華，樂嘉陵) 222
馬赫數為4的超燃發動機碳氫燃料點火試驗 (張彎洲，樂嘉陵，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傳熱的數值模擬 (趙國柱，宋文艷，張若凌，樂嘉陵) 244
吸氣式高超聲速飛行器機體推進一體化技術研究進展 ，賀偉，樂嘉陵) 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
強制轉捩對高超聲速進氣道性能影響 (易淼榮，趙慧勇，樂嘉陵) 280
亞聲速橫向氣流中液體射流破碎過程的直接模擬 (劉日超，樂嘉陵，楊順華，鄭忠華，宋文艷，黃淵) 288
電加熱圓管內流動的自然轉捩過程研究 (張若凌，樂嘉陵) 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結構大渦模擬研究 (周瑜，樂嘉陵，陳柳君，黃淵) 333
軸向三級旋流燃燒室流場結構大渦模擬 (周瑜，樂嘉陵，陳柳君，黃淵) 342
Design and analysis osculating general curved cone waverider (Xuzhao He，Jialing Le，Si Qin) 351
附錄 樂嘉陵院士發表的論文 358