Ignition delay times of Jet A-1 fuel: Measurements in a high-pressure shock tube and a rapid compression machine

2017 ◽  
Vol 36 (3) ◽  
pp. 3695-3703 ◽  
Author(s):  
A.R. De Toni ◽  
M. Werler ◽  
R.M. Hartmann ◽  
L.R. Cancino ◽  
R. Schießl ◽  
...  
Keyword(s):  
High Pressure ◽  
Shock Tube ◽  
Ignition Delay ◽  
Rapid Compression Machine ◽  
Pressure Shock ◽  
Ignition Delay Times ◽  
Delay Times ◽  
Rapid Compression

Ignition delay times of methane fuels at thrust chamber conditions in an ultra-high-pressure shock tube

2022 ◽  
Author(s):  
Michael Pierro ◽  
Andrew Laich ◽  
Justin J. Urso ◽  
Cory Kinney ◽  
Subith Vasu ◽  
...  
Keyword(s):  
High Pressure ◽  
Shock Tube ◽  
Ignition Delay ◽  
Pressure Shock ◽  
Thrust Chamber ◽  
Ultra High Pressure ◽  
Ignition Delay Times ◽  
Delay Times

The effect of diluent gases on ignition delay times in the shock tube and in the rapid compression machine

2007 ◽  
Vol 151 (1-2) ◽  
pp. 289-302 ◽  
Author(s):  
J. Würmel ◽  
E.J. Silke ◽  
H.J. Curran ◽  
M.S. Ó Conaire ◽  
J.M. Simmie
Keyword(s):  
Shock Tube ◽  
Ignition Delay ◽  
Rapid Compression Machine ◽  
Ignition Delay Times ◽  
Delay Times ◽  
Rapid Compression

Impact of CO2 Dilution on Ignition Delay Times of Full Blend Gasolines in a Rapid Compression Machine

2021 ◽  
Author(s):  
Prasanna Chinnathambi ◽  
Chaitanya Wadkar ◽  
Soumya Gudiyella ◽  
Fadi Estefanous ◽  
Elisa Toulson
Keyword(s):  
Ignition Delay ◽  
Rapid Compression Machine ◽  
Ignition Delay Times ◽  
Delay Times ◽  
Rapid Compression

High Pressure Ignition of Boron in Reduced Oxygen Atmospheres

1995 ◽  
Vol 418 ◽  
Author(s):  
R. O. Foelsche ◽  
M. J. Spalding ◽  
R. L. Burton ◽  
H. Krier
Keyword(s):  
High Pressure ◽  
Water Vapor ◽  
Shock Tube ◽  
Ignition Delay ◽  
Peak Pressure ◽  
Reflected Shock ◽  
Ignition Delay Times ◽  
Fluorine Compounds ◽  
Delay Times ◽  
Tube Study

AbstractBoron ignition delay times for 24 μm diameter particles have been measured behind the reflected shock at a shock tube endwall in reduced oxygen atmospheres and in a combustion bomb at higher pressures in the products of a hydrogen/oxygen/nitrogen reaction. The shock tube study independently varies temperature (1400 – 3200 K), pressure (8.5, 34 atm), and ignition-enhancer additives (water vapor, fluorine compounds). A combustion chamber is used at a peak pressure of 157 atm and temperature in excess of 2800 K to study ignition delays at higher pressures than are possible in the shock tube.

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