Numerical Investigation of the Unsteady Flow in a Transonic Compressor with Curved Rotors
pressure fluctuation、aerodynamic interaction、flow fields
21
V2(航空)
国家自然科学基金506460210;Chinese Specialized Research Fund for the Doctoral Program of Higher Education20060213007;Development Program for Outstanding Young Teachers in Harbin Institute of TechnologyHITQNJS.2006.046
2008-06-24(万方平台首次上网日期,不代表论文的发表时间)
共8页
97-104