10.13224/j.cnki.jasp.2017.05.020
Simulation on effect of throat contraction ratio and strake stagger angle on flow field and aerodynamic performance of scrampressor
aerodynamic performance、pressure recovery coefficient、pressure ratio、flow field、compression ramp、shock wave、methods of、flow path
32
V231.1(航空发动机(推进系统))
Fundamental Research Funds for the Central Universities3132016205;National Natural Science Foundation of China51506020;Natural Science Foundation of Liaoning Province2015020636;Program for Liaoning Innovative Research Team in UniversityLT2015004
2017-07-06(万方平台首次上网日期,不代表论文的发表时间)
共12页
1183-1194