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第1 期 发动机 固体火箭喷管颗粒尺寸分级两相跨音速流场计算……… ’…………………………………………··侯 晓 何洪庆 蔡体敏 吴心平(1) 潜人喷管背壁流场模拟显示…………………………………黄志柱 何国强 吴心平(9) 具有拉伐尔喷口的离心喷嘴雾化锥角调整方法……………
Phase 1 engine solid rocket lance particle size grading two-phase transonic flow field calculation ......... ’................................................ · Hou Xiao He Hongqing Cai Tiomin Wu Xinping (1) People nozzle back wall flow field simulation shows ....................................... Huang Zhizhu He Guoqiang Wu Xinping (9) Centrifugal nozzle with Laval nozzle atomization cone angle adjustment method ...............