An experimental investigation into the transonic flow-fields of tandem cavities

1998 ◽  
Author(s):  
D. Bray
Keyword(s):  
Experimental Investigation ◽  
Transonic Flow ◽  
Flow Fields

Effect of nonequilibrium condensation of moist air on transonic flow fields

2000 ◽  
Vol 9 (1) ◽  
pp. 37-44 ◽  
Author(s):  
Katsumi Shimamoto ◽  
Shigeru Matsuo ◽  
Toshiaki Setoguchi
Keyword(s):  
Transonic Flow ◽  
Flow Fields ◽  
Moist Air ◽  
Nonequilibrium Condensation

Experimental investigation and optimization of proton exchange membrane fuel cell using different flow fields

Energy ◽  
2020 ◽  
pp. 119313
Author(s):  
Aezid-Ul-Hassan Najmi ◽  
Ikechukwu S. Anyanwu ◽  
Xu Xie ◽  
Zhi Liu ◽  
Kui Jiao
Keyword(s):  
Experimental Investigation ◽  
Fuel Cell ◽  
Proton Exchange Membrane ◽  
Flow Fields ◽  
Proton Exchange ◽  
Exchange Membrane

REVIEW—Progress in Numerical Turbomachinery Analysis

1976 ◽  
Vol 98 (4) ◽  
pp. 592-606 ◽  
Author(s):  
David Japikse
Keyword(s):  
Numerical Analysis ◽  
Steady Flow ◽  
Transonic Flow ◽  
Three Dimensional ◽  
Flow Fields ◽  
Design Methods ◽  
Two Dimensional ◽  
Wide Spread ◽  
The Past ◽  
Turbomachinery Design

Progress achieved in numerical analysis during the past decade now permits the turbo-machinery designer to carry out a wide variety of inviscid, steady flow, two-dimensional calculations for compressible sybsonic and transonic flow fields, including some strongly diffusing flows. Three-dimensional (including viscosity) calculations are under development and should find wide spread use as analysis tools during the next decade. This review offers an introduction to recent advances in numerical turbomachinery design methods guided by the author’s design usage of several of the techniques reported.

Experimental Study of Effects of Bowed Blade on the Flow Field in a Cantilevered Stator Passage

2014 ◽  
Author(s):  
Ju Luo ◽  
Jun Hu ◽  
Zhiqiang Wang ◽  
Baofeng Tu
Keyword(s):  
Experimental Study ◽  
Experimental Investigation ◽  
Flow Field ◽  
Maximum Flow ◽  
Suction Side ◽  
Flow Fields ◽  
Compressor Blade ◽  
Blade Passage ◽  
Hole Pressure ◽  
Passage Vortex

This paper presents experimental investigation conducted on a 2-stage low speed axial research compressor with cantilevered stator vanes. Flow fields at four different axial locations in the radial stacking and bowed stator passage were measured at maximum flow point and near stall point using 4 five-hole pressure probes. The aim of the work is to study the effects of the bowed stators with hub clearance on the flow field of compressor blade passage. The investigations were conducted with the first stage of the compressor. The hub clearances of both original and bowed stators are 1.1% of span. The results show that the scale of the separation vortex, the hub leakage vortex and the lower passage vortex in the bowed blade passage becomes much smaller and the hub leakage vortex is closer to the suction side at near stall point, which causes a much smaller mixing loss in the blade passage.

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