Condensation of Water Vapor in the Shock Tube Below 150°K

1951 ◽  
Vol 22 (2) ◽  
pp. 233-233 ◽  
Author(s):  
P. Wegener ◽  
G. Lundquist
Keyword(s):  
Water Vapor ◽  
Shock Tube

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 ignition of AL/MG alloys in water vapor and argon

1993 ◽  
Vol 7 (2) ◽  
pp. 154
Author(s):  
ThomasW. Megli ◽  
Herman Krier ◽  
RodneyL. Burton
Keyword(s):  
Water Vapor ◽  
Shock Tube ◽  
Mg Alloys ◽  
Al Mg Alloys
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