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Aerodynamic Sweeping Study and Design for Transonic Compressor Rotor blades

文献类型:期刊论文

作者N.X. Chen ; H.W. Zhang ; W.G Huang
刊名JOURNAL OF THERMAL SCIENCE
出版日期2010
卷号19期号:4页码:295,299
关键词Aerodynamic optimization blade sweep transonic compressor rotor
英文摘要The objective of the present paper is to study the sweep effect on the blade design performance of a transonic compressor rotor. The baseline to be modified and swept is a designed well efficient transonic single rotor compressor. The first part of the present study is concerning the sweep effect with straight leading edge. In this case fixing the hub section the swept blade is formed by tilting the leading edge with whole blade forwards and backwards axially. The second part is to use an optimization strategy with simple gradient-based optimum-searching method and multi-section blade parameterization technique to search and generate an optimal swept rotor with curved arbitrary leading edge. Its adiabatic efficiency is a little bit greater than that of the reference un-swept rotor.
WOS记录号WOS:000279656900002
公开日期2013-01-06
源URL[http://ir.etp.ac.cn/handle/311046/51627]  
专题工程热物理研究所_Journal of Thermal Science_期刊论文
推荐引用方式
GB/T 7714
N.X. Chen,H.W. Zhang,W.G Huang. Aerodynamic Sweeping Study and Design for Transonic Compressor Rotor blades[J]. JOURNAL OF THERMAL SCIENCE,2010,19(4):295,299.
APA N.X. Chen,H.W. Zhang,&W.G Huang.(2010).Aerodynamic Sweeping Study and Design for Transonic Compressor Rotor blades.JOURNAL OF THERMAL SCIENCE,19(4),295,299.
MLA N.X. Chen,et al."Aerodynamic Sweeping Study and Design for Transonic Compressor Rotor blades".JOURNAL OF THERMAL SCIENCE 19.4(2010):295,299.

入库方式: OAI收割

来源:工程热物理研究所

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