| Citation: | SUN Peng, FENG Guo-tai. Analysis of flow loss induced by inlet total pressure distortion in a small fan[J]. Journal of Aerospace Power, 2007, 22(2): 245-250. |
| [1] |
Peaeson H,McKenzie A.Wakes in axial compressors[J].Journal of the Royal Aeronautical Society,1959,63:154-186.
|
| [2] |
Luedke J G.Use of nonlinear volterra theory in predicting the propagation of non-uniform flow through an axial compressor[D].Master Thesis,Virginia Polytechnic Institute and State University,2001.
|
| [3] |
Wallace R M.Modal response of a transonic fan blade to periodic inlet pressure distortion[D].Master Thesis,Virginia Polytechnic Institute and State University,2003.
|
| [4] |
Rabe D C,Williams C,Hah C.Inlet flow distortion and unsteady bladeresponse in a transonic axial-compressor rotor[R].ISABE 99-7297,1999.
|
| [5] |
Denton J D.Loss mechanisms in turbomachines[J].ASME Journalof Turbomachinery,1993,115(4):621-656.
|