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Ignition of SiH4-H2-O2-N2 behind reflected shock wavesThe ignition of mixtures of silane, hydrogen, and oxygen diluted with nitrogen was studied in a chemical kinetic shock tube. Ignition delay time measurements were made behind reflected shock waves at pressures of 1.25 atm and 1.35 atm and temperatures ranging from approximately 800 K to 1050 K for two mixtures with silane-oxygen equivalence ratios of 1.0 and 0.5, respectively. Enhancement of the ignition by use of silane was observed experimentally by the failure of a similar mixture containing only hydrogen, oxygen, and nitrogen to ignite during the maximum test time available for these test conditions.
Document ID
19830010456
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Mclain, A. G.
(NASA Langley Research Center Hampton, VA, United States)
Jachimowski, C. J.
(NASA Langley Research Center Hampton, VA, United States)
Rogers, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
L-15534
NASA-TP-2114
NAS 1.60:2114
Report Number: L-15534
Report Number: NASA-TP-2114
Report Number: NAS 1.60:2114
Accession Number
83N18727
Funding Number(s)
PROJECT: RTOP 505-43-83-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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