Shock-Tube Study of the Effects of Nitrogen and Water Vapor on Recombination in the Hydrogen-Oxygen System

1969 ◽  
Vol 12 (5) ◽  
pp. I-176 ◽  
Author(s):  
R. W. Getzinger
Keyword(s):  
Water Vapor ◽  
Shock Tube ◽  
Oxygen System ◽  
Tube Study

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.

Shock tube study of decomposition of nitric oxide at high temperatures

1975 ◽  
Vol 15 (1) ◽  
pp. 809-822 ◽  
Author(s):  
M. Koshi ◽  
H. Ando ◽  
M. Oya ◽  
T. Asaba
Keyword(s):  
Nitric Oxide ◽  
Shock Tube ◽  
High Temperatures ◽  
Tube Study

Shock-tube study of allene pyrolysis

1987 ◽  
Vol 91 (24) ◽  
pp. 6291-6296 ◽  
Author(s):  
C. H. Wu ◽  
R. D. Kern
Keyword(s):  
Shock Tube ◽  
Tube Study

A shock tube study of the autoignition characteristics of RP-3 jet fuel

2015 ◽  
Vol 35 (3) ◽  
pp. 3151-3158 ◽  
Author(s):  
Changhua Zhang ◽  
Bin Li ◽  
Fan Rao ◽  
Ping Li ◽  
Xiangyuan Li
Keyword(s):  
Shock Tube ◽  
Jet Fuel ◽  
Tube Study
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