Measurement, Diagnostic Techniques and Initial Shock Tube Experiments

Author(s):  
Padmanabha Vivek ◽  
T. G. Sitharam
2020 ◽  
Vol 117 (7) ◽  
pp. 3451-3460 ◽  
Author(s):  
Samuel Barak ◽  
Ramees K. Rahman ◽  
Sneha Neupane ◽  
Erik Ninnemann ◽  
Farhan Arafin ◽  
...  

Soot emissions in combustion are unwanted consequences of burning hydrocarbon fuels. The presence of soot during and following combustion processes is an indication of incomplete combustion and has several negative consequences including the emission of harmful particulates and increased operational costs. Efforts have been made to reduce soot production in combustion engines through utilizing oxygenated biofuels in lieu of traditional nonoxygenated feedstocks. The ongoing Co-Optimization of Fuels and Engines (Co-Optima) initiative from the US Department of Energy (DOE) is focused on accelerating the introduction of affordable, scalable, and sustainable biofuels and high-efficiency, low-emission vehicle engines. The Co-Optima program has identified a handful of biofuel compounds from a list of thousands of potential candidates. In this study, a shock tube was used to evaluate the performance of soot reduction of five high-performance biofuels downselected by the Co-Optima program. Current experiments were performed at test conditions between 1,700 and 2,100 K and 4 and 4.7 atm using shock tube and ultrafast, time-resolve laser absorption diagnostic techniques. The combination of shock heating and nonintrusive laser detection provides a state-of-the-art test platform for high-temperature soot formation under engine conditions. Soot reduction was found in ethanol, cyclopentanone, and methyl acetate; conversely, an α-diisobutylene and methyl furan produced more soot compared to the baseline over longer test times. For each biofuel, several reaction pathways that lead towards soot production were identified. The data collected in these experiments are valuable information for the future of renewable biofuel development and their applicability in engines.


1979 ◽  
Vol 10 (17) ◽  
Author(s):  
E. A. DORKO ◽  
N. R. PCHELKIN ◽  
J. C. III WERT ◽  
G. W. MUELLER
Keyword(s):  

Author(s):  
H-D Kim ◽  
Y-H Kweon ◽  
T Setoguchi

The propagation of the impulsive wave discharged from the inclined exit of a tube is investigated using a shock tube experiment and by numerical computations. The pressure histories and wavefront geometries of the impulsive wave propagating outside the exits of the tube with several different configurations are analysed for the range of an initial shock wave Mach number between 1.1 and 1.4. In the shock tube experiments, the impulsive waves are visualized by a Schlieren optical system for the purpose of validation of computational work. Computations using the two-dimensional, unsteady, compressible, Euler equations are carried out to represent the experimental impulsive waves. The results obtained show that the inclination angle of the tube exit reduces the magnitude of the impulsive wave and affects the wavefront geometry of the impulsive wave. It is also found that the propagation direction and magnitude of the impulsive wave depend on the Mach number of the initial shock wave, while the impulsive waveform does not significantly vary with the Mach number of the initial shock wave. The computed results obtained predict the experimental ones with quite good accuracy.


1979 ◽  
Vol 83 (2) ◽  
pp. 297-302 ◽  
Author(s):  
Ernest A. Dorko ◽  
Nicholas R. Pchelkin ◽  
John C. Wert ◽  
Gerhard W. Mueller
Keyword(s):  

1968 ◽  
Vol 11 (43) ◽  
pp. 116-124 ◽  
Author(s):  
Kiyohiro TAJIMA ◽  
Eisuke OUTA ◽  
Goro NAKADA

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