C/SiC复合材料在超燃冲压发动机中的应用研究进展
马青松1, 刘海韬1,2, 潘余2, 刘卫东2, 陈朝辉1

Research Progress on the Application of C/SiC Composites in Scramjet
MA Qing-Song1, LIU Hai-Tao1,2, PAN Yu2, LIU Wei-Dong2, CHEN Zhao-Hui1
图2 试验后的前缘半径为0.75 mm的进气道唇口 [ 14 ]
Fig. 2 Leading edge sample 0.75 mm radius after test [ 14 ]