The interaction ~,f ~seous sbock and detonation waves with liquid layer~ has been studied in a shock tube in order to elucidate the i~Jitian mechanism in heterogeneous systems consisting of a liquid fuel film and a gaseous oxidizer. It was shown t~'~tt after passage of the shock front over the liqui
Rate of ionization behind shock waves in air
โ Scribed by S.C. Lin
- Publisher
- Elsevier Science
- Year
- 1961
- Tongue
- English
- Weight
- 735 KB
- Volume
- 6
- Category
- Article
- ISSN
- 0032-0633
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๐ SIMILAR VOLUMES
The thermal decomposition of acetylene has been studied in the temperature and pressure regimes of 1900-2500 K and 0.3-0.55 atm using a shock tube coupled to a time-of-flight mass spectrometer. A series of mixtures varying from 1.0-6.2% CzHz diluted in a Ne-Ar mixture yielded a carbon atom density r
The pyrolysis of benzene was studied in the temperature and pressure range of 1400-2200K and 0.25-0.81 arm using a shock tube coupled to a time-of-flight mass spectrometer. The mixtures employed were 2.1 and 5% benzene diluted with neon, which yielded a carbon atom density range of (1.6-7.9) x 1017
Rates of NF, thermal decomposition in the temperature range 1450-2050 K and pressure range 1.2-4.2 atm were measured by a shock tube technique. NF? decomposition was monitored by UV absorption of the produced NFI radicals. The bimolecular rate constant of the NF3 decomposition reaction essentially d
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