Shock tube study of ignition delay times in methaneoxygennitrogenargon mixtures

1976 ◽  
Vol 27 ◽  
pp. 377-381 ◽  
Author(s):  
A. Grillo ◽  
M.W. Slack
1995 ◽  
Vol 418 ◽  
Author(s):  
R. O. Foelsche ◽  
M. J. Spalding ◽  
R. L. Burton ◽  
H. Krier

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.


2015 ◽  
Vol 35 (1) ◽  
pp. 231-239 ◽  
Author(s):  
Matthew F. Campbell ◽  
Shengkai Wang ◽  
Christopher S. Goldenstein ◽  
R. Mitchell Spearrin ◽  
Andrew M. Tulgestke ◽  
...  

2009 ◽  
Vol 32 (1) ◽  
pp. 477-484 ◽  
Author(s):  
D.R. Haylett ◽  
P.P. Lappas ◽  
D.F. Davidson ◽  
R.K. Hanson

2016 ◽  
Vol 164 ◽  
pp. 152-163 ◽  
Author(s):  
Batikan Koroglu ◽  
Owen M. Pryor ◽  
Joseph Lopez ◽  
Leigh Nash ◽  
Subith S. Vasu

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