scholarly journals Aspect-Ratio and Reynolds-Number Effects on Short-Span Cross-Flow Impellers without Casings

2006 ◽  
Vol 49 (4) ◽  
pp. 1197-1205 ◽  
Author(s):  
Jiro FUNAKI ◽  
Nobuyuki KIMATA ◽  
Motohide HISADA ◽  
Katsuya HIRATA
2007 ◽  
Vol 73 (736) ◽  
pp. 2514-2523
Author(s):  
Jiro FUNAKI ◽  
Nobuyuki KIMATA ◽  
Motohide HISADA ◽  
Katuya HIRATA

Author(s):  
Jamison L. Szwalek ◽  
Carl M. Larsen

In-line vibrations have been noted to have an important contribution to the fatigue of free spanning pipelines. Still, in-line contributions are not usually accounted for in current VIV prediction models. The present study seeks to broaden the current knowledge regarding in-line vibrations by expanding the work of Aronsen (2007) to include possible Reynolds number effects on pure in-line forced, sinusoidal oscillations for four Reynolds numbers ranging from 9,000 to 36,200. Similar tests were performed for pure cross-flow forced motion as well, mostly to confirm findings from previous research. When experimental uncertainties are accounted for, there appears to be little dependence on Reynolds number for all three hydrodynamic coefficients considered: the force in phase with velocity, the force in phase with acceleration, and the mean drag coefficient. However, trends can still be observed for the in-line added mass in the first instability region and for the transition between the two instability regions for in-line oscillations, and also between the low and high cross-flow added mass regimes. For Re = 9,000, the hydrodynamic coefficients do not appear to be stable and can be regarded as highly Reynolds number dependent.


2006 ◽  
Vol 2006.81 (0) ◽  
pp. _13-8_
Author(s):  
Jiro FUNAKI ◽  
Motohide HISADA ◽  
Nobuyuki KIMATA ◽  
Katsuya HIRATA

Author(s):  
Ravi S. Prasher ◽  
John Dirner ◽  
Je-Young Chang ◽  
Alan Myers ◽  
David Chau ◽  
...  

Experimental results of the thermal and hydraulic performances of silicon-based, low aspect ratio micro-pin-fin cold plates under cross flow conditions are reported. The pins were both circular and square in shape with dimensions (diameter for circular and sides for square) ranging from 50 to 150 μm. The test chip contained 20 integral 75×75 μm temperature sensors which were used to determine the thermal resistance (K W-1) of the cold plates. The experiments were conducted using water, over a Reynolds number (Re) ranging from 40 to 1000. The data show that the average Nusselt number (Nu) based on the fin diameter varies as Re0.84 for Re < 100 and as Re0.73 for Re > 100, where Re is the Reynolds number based on maximum velocity and the fin diameter. Analysis of the Fanning friction factor (f) data shows that f varies as Re-1.35 for Re < 100 and as Re-0.1 for Re > 100.


2006 ◽  
Vol 129 (2) ◽  
pp. 141-153 ◽  
Author(s):  
Ravi S. Prasher ◽  
John Dirner ◽  
Je-Young Chang ◽  
Alan Myers ◽  
David Chau ◽  
...  

Experimental results of the thermal and hydraulic performances of silicon-based, low aspect ratio micropin-fin cold plates under cross flow conditions are reported. The pins were both circular and square in shape with dimensions (diameter for circular and sides for square) ranging from 50μm to 150μm. The test chip contained 20 integral 75×75μm temperature sensors which were used to determine the thermal resistance (KW−1) of the cold plates. The experiments were conducted using water, over a Reynolds number (Re) ranging from 40 to 1000. The data show that the average Nusselt number (Nu) based on the fin diameter varies as Re0.84 for Re<100 and as Re0.73 for Re>100, where Re is the Reynolds number based on maximum velocity and the fin diameter. Analysis of the Fanning friction factor (f) data shows that f varies as Re−1.35 for Re<100 and as Re−0.1 for Re>100.


1964 ◽  
Vol 86 (3) ◽  
pp. 236-242
Author(s):  
J. H. Horlock ◽  
R. Shaw ◽  
D. Pollard ◽  
A. Lewkowicz

A series of tests on guide vane and compressor cascades is reported. The Reynolds number was varied in the guide vane cascade tests, and the Reynolds number and the cascade aspect ratio were varied in the compressor cascade tests. The substantial laminar separation observed in the compressor cascades at high aspect ratio (and low Reynolds number) was suppressed in the cascade tests at low aspect ratio, 2:1. Effects of Reynolds number variation on the performance of a single stage axial flow compressor are also given, and compared with predictions of performance using the cascade tests. Calculations of laminar separation points agree quite well with the experimental observations. It appears that transition due to laminar boundary layer instability is unlikely to occur on compressor blades, in the normal operating range of Reynolds number.


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