Structural mass prediction in conceptual design of blended-wing-body aircraft
prediction method、finite element analysis、structural component、structure analysis、structural feature、conceptual design
32
TP1;TG1
This study was supported by the National Natural Science Foundation of China11432007
2019-12-26(万方平台首次上网日期,不代表论文的发表时间)
共11页
2455-2465