Numerical and Experimental Study of Turbulent Mixing in Colorless Distributed Combustion Systems

2012 ◽  
Author(s):  
Husam Abdul-Rahman ◽  
Farhad Jaberi ◽  
Ahmed Khalil ◽  
Ashwani Gupta
Keyword(s):  
Experimental Study ◽  
Turbulent Mixing ◽  
Combustion Systems ◽  
Colorless Distributed Combustion

scholarly journals An experimental study of reactive turbulent mixing

1977 ◽  
Author(s):  
L. COOPER ◽  
C. MAREK ◽  
R. STREHLOW
Keyword(s):  
Experimental Study ◽  
Turbulent Mixing

scholarly journals Experimental Study on The Turbulent Mixing between Main Channel and Flood Plain Flows

1992 ◽  
Vol 36 ◽  
pp. 139-144
Author(s):  
Hirotake IMAMOTO ◽  
Taisuke ISHIGAKI ◽  
Yasunori MUTOH
Keyword(s):  
Experimental Study ◽  
Turbulent Mixing ◽  
Flood Plain ◽  
Main Channel

scholarly journals Rayleigh–Taylor turbulent mixing evolution under a shock influence

2000 ◽  
Vol 18 (2) ◽  
pp. 155-161 ◽  
Author(s):  
Yu.A. KUCHERENKO ◽  
A.P. PYLAEV ◽  
V.D. MURZAKOV ◽  
V.N. POPOV ◽  
V.E. SAVEL'EV ◽  
...  
Keyword(s):  
Experimental Study ◽  
Solid Surface ◽  
Turbulent Mixing ◽  
Initial Perturbation ◽  
Density Ratio ◽  
Internal Working ◽  
Metal Plates ◽  
Impulse Duration ◽  
Rayleigh Taylor Instability ◽  
The Impact

At the installation SOM, the experimental study of the impulse acceleration influence on the behavior of the turbulized layer obtained as a result of Rayleigh–Taylor instability (RTI) action on the system of two different density liquids with the density ratio n = 3, has been performed. After application of impulse acceleration the systems were moving according to inertia, and by using the light method the coordinates of penetration of the heavier liquid into the lighter one and vice versa were determined. The liquids studied were placed inside the ampoule that had internal working sizes (54 × 64 × 120) mm3. There were initial accidental perturbations like a rough solid surface at the interface and the width of the initial perturbation zone was L0 = 2.3 mm. The moving ampoule blow against metal plates created the impulse acceleration. The relative impulse acceleration was δg/g11 = 22.2–66.6 where g11 is the ampoule acceleration before the impact, the impulse duration was varied from 0.27 ms to 0.096 ms. The results concerned with the turbulized layer extension after the impulse acceleration action were obtained.

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