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- W2364154654 abstract "According to the requirements of collective capability,a low-pressure compressor such as fan/compressor worked at low Reynolds Number was designed by the through flow program.The design including configuration of flow passage and the blade geometry of each blade row was finished.Then,the fan/compressor was calculated by three-dimension numerical simulation software named NUMECA(Numerical Mechanics Application).Referring to aerodynamic design circulation,the configurations of flow passage and blade profile geometry of fan/compressor were confirmed;furthermore,based on the 12km,0.6Ma flight condition the aerodynamic parameters were calculated at 100%,95% corrected speed in order to evaluate the cruise performance and the feature of flow field.On the other side,the characteristic curve of 86.6%,80% corrected speed under the condition of the standard ground atmosphere was obtained by calculation.It could be used to review the fan/compressor performance operated in maximum region of its ground take-off.The three-dimension numerical simulation result indicates that the design requirements of bypass duct have been realized completely,and the design requirements of core duct were almost realized expects its efficiency." @default.
- W2364154654 created "2016-06-24" @default.
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- W2364154654 date "2007-01-01" @default.
- W2364154654 modified "2023-09-26" @default.
- W2364154654 title "Aerodynamic Design of Fan/Compressor Operated at Low Reynolds Number" @default.
- W2364154654 hasPublicationYear "2007" @default.
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