摘要
分析了虚拟固体燃料冲压发动机连管试验的基础技术,归纳了其试验器方案设计任务。重点探讨了连管试验器各部件的设计方案。
The fundamental technology for connecting tube test of virtual solid -fuel ramjet is analyzed, and the design specification of tester concept is concluded. The design concepts of various components of tester are primarily discussed.
出处
《航空发动机》
2007年第3期15-17,共3页
Aeroengine