Analysis of the core driven fan stage with compact aerodynamic configuration
Coll.of Energy and Power Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China;Coll.of Energy and Power Engineering, Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China
[2] 张鑫,刘宝杰.核心机驱动风扇级的气动设计特点分析[J].航空动力学报,0,5(2):434-442. [3] 支钟和.变循环发动机的进展[J].江苏航空,2,2:13-14. [4] French M W, Allen G L.NASA VCE test bed engine aerodynamic performance characteristics and results[R].AIAA 81-1594. [5] Vdoviak J W, Ebacker J A.VCE test bed engine for supersonic cruise research[C].USA: NASA Conference Publication8,9. [6] 方昌德.变循环发动机及其关键技术[J].国际航空杂志,4,7:49-51. [7] Gallimore S J, Bolger J J, Cumpsty N A, et al.The use of sweep and dihedral in multistage axial flow compressor blading—part I:university research and methods development[R].ASME 2003-GT-30328.