Numerical and experimental observation of three-dimensional unsteady shock wave structures

1997 ◽  
Author(s):  
E. Timofeev ◽  
K. Takayama ◽  
P. Voinovich ◽  
E. Timofeev ◽  
K. Takayama ◽  
...  
Keyword(s):  
Shock Wave ◽  
Experimental Observation ◽  
Three Dimensional ◽  
Shock Wave Structures

scholarly journals Three-dimensional graphic display for the shock wave structures using image processing.

1988 ◽  
Vol 8 (30) ◽  
pp. 289-292
Author(s):  
Shohachi YASU ◽  
Teiichi TAMAKI ◽  
Susumu NAGANO ◽  
Masato USHIKUSA ◽  
Takao KASHIWAGI
Keyword(s):  
Shock Wave ◽  
Image Processing ◽  
Three Dimensional ◽  
Graphic Display ◽  
Shock Wave Structures

Experimental observation of nonuniversal behavior of the conductivity exponent for three-dimensional continuum percolation systems

1986 ◽  
Vol 34 (10) ◽  
pp. 6719-6724 ◽  
Author(s):  
Sung-Ik Lee ◽  
Yi Song ◽  
Tae Won Noh ◽  
Xiao-Dong Chen ◽  
James R. Gaines
Keyword(s):  
Experimental Observation ◽  
Three Dimensional ◽  
Continuum Percolation

Unsteady Three-Dimensional Analysis of Inlet Distortion in a Transonic Fan

2006 ◽  
Author(s):  
Peng Sun ◽  
Guotal Feng
Keyword(s):  
Shock Wave ◽  
Total Pressure ◽  
Large Scale ◽  
Three Dimensional ◽  
Navier Stokes ◽  
Inlet Distortion ◽  
Flow Loss ◽  
Large Scale Vortex ◽  
Total Temperature ◽  
Transonic Fan

A time-accurate three-dimensional Navier-Stokes solver of the unsteady flow field in a transonic fan was carried out using "Fluent-parallel" in a parallel supercomputer. The numerical simulation focused on a transonic fan with inlet square wave total pressure distortion and the analysis of result consisted of three aspects. The first was about inlet parameters redistribution and outlet total temperature distortion induced by inlet total pressure distortion. The pattern and causation of flow loss caused by pressure distortion in rotor were analyzed secondly. It was found that the influence of distortion was different at different radial positions. In hub area, transportation-loss and mixing-loss were the main loss patterns. Distortion not only complicated them but enhanced them. Especially in stator, inlet total pressure distortion induced large-scale vortex, which produced backflow and increased the loss. While in casing area, distortion changed the format of shock wave and increased the shock loss. Finally, the format of shock wave and the hysteresis of rotor to distortion were analyzed in detail.

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