A new numerical simulation method of high reynolds number flow around a cylinder

1998 ◽  
Vol 158 (3-4) ◽  
pp. 357-366 ◽  
Author(s):  
T. Guo ◽  
Y.T. Chew ◽  
S.C. Luo ◽  
M.D. Su
2004 ◽  
Vol 13 (5) ◽  
pp. 712-719 ◽  
Author(s):  
Zhou Xiao-Yang ◽  
Shi Bao-Chang ◽  
Wang Neng-Chao

1995 ◽  
Vol 2 (1) ◽  
pp. 23-32
Author(s):  
Tsutomu adachi

In this paper, first, the principle, structures, operations, and performances of the cryogenic wind tunnel are described. By changing the pressure, temperature and velocity of gas a high Reynolds-number flow(5×104<Re<107)can be obtained. From the research results, a high Reynolds-number flow with comparatively low power, LN consumptions was attained. It was with Mach-number independent of each other, o show some examples of high Reynolds-number flow, the effects of surface roughness and grooves on the surface of a cylinder on the flow are measured using models with various values of roughness and size. A model test of an airship was also conducted. With the high Reynolds-number flow, the thickness of the boundary layer becomes thinner. Then the surface conditions of a body have great effect on the flow phenomena and on the drag of the body. Some attempts to reduce the drag of the body were shown.


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