Method for utilizing PIV to investigate high curvature and acceleration boundary layer flows around the compressor blade leading edge
boundary、blade、method、layer、edge、high、acceleration、around、compressor、curvature
35
TP391.9;R445.2;R816.1
2023-03-08(万方平台首次上网日期,不代表论文的发表时间)
共17页
72-88