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Mechanism of ignition in shock wave interactions with reactive liquid dropletsA detailed qualitative analysis of the processes leading to the explosive ignition of a reactive liquid droplet that is suspended in a gas-phase oxidizer and subjected to the passage of a shock wave, is presented. The interval of time between shock wave passage and ignition is described by identifying a two-stage process which consists of a period of relative reactive dormancy that is followed by a chemical induction period leading to the thermal explosion of reactant that has been stripped from the liquid drop, vaporized, and mixed with the gas-phase oxidizer. The results of first-order calculations based on this model are presented and compared with experimental data for diethlcyclohexane drops in oxygen.
Document ID
19750034280
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pierce, T. H.
Kauffman, C. W.
Nicholls, J. A.
(Michigan, University Ann Arbor, Mich., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
AIAA PAPER 75-163
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 20, 1975
End Date: January 22, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A18352
Funding Number(s)
CONTRACT_GRANT: NGL-23-005-336
Distribution Limits
Public
Copyright
Other

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