Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Sheng Zhou"'
Publikováno v:
Volume 12: Vibration, Acoustics and Wave Propagation.
Under inlet total pressure distortion, forced response of compressor blades poses a threat to aircraft propulsion system. Research on blade dynamic response is premise and basis for high-cycle fatigue life analysis. Blades of a compressor first rotor
Publikováno v:
Volume 7: Structures and Dynamics, Parts A and B.
A time domain numerical approach is carried out to enhance the understanding of three dimensional blade row aeroelastic characteristics under the parallel computation. The vibration energy of unsteady aerodynamic force on the entire blade row is inve
Autor:
Sheng Zhou, Peng Shan
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
This paper is Part I of a comprehensive study on the blade leading edge sweep/bend of supersonic and transonic axial compressors. The objective of the paper is to develop an analytical shock surface model which links a blade leading edge with the 3-D
Autor:
Ren-Jing Cao, Sheng Zhou
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
Rotating stall phenomenon is usually characterized by 3D aerodynamic stability behavior. The earlier models mainly considered the flow effects in terms of 1D and 2D spatial variables. In order to involve the characteristics of the 3D flow of the comp
Publikováno v:
Journal of Turbomachinery; Apr2011, Vol. 133 Issue 2, p21014.1-21014.6, 6p, 8 Graphs
Publikováno v:
Journal of Fluids Engineering; Apr2008, Vol. 130 Issue 4, p2:1-2:9, 9p, 1 Diagram, 8 Graphs
Publikováno v:
Journal of Turbomachinery; Apr2008, Vol. 130 Issue 2, p1-7, 7p, 4 Diagrams, 1 Chart, 8 Graphs