Uncertainty analysis of deflagration-to-detonation run-up distance

J. Li, W. H. Lai, K. Chung, Frank K. Lu

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Three methods were adopted to estimate the deflagration-to-detonation run-up distance in a smooth tube, which comprises of (1) the measurement of the propagation speed of pressure or combustion waves compared with the C-J detonation speed, (2) the time of the onset of detonation by the emission of visible light and the trajectory of pressure wave or combustion waves, and (3) the trajectory intersection with the presence of retonation wave. A nonstationary cross-correlation technique was applied to evaluate the uncertainty in estimating the run-up distance. Evaluation of the pressure wave (pressure wave speed or the pressure wave trajectory) appears to be more suitable to determine the deflagration- to-detonation run-up distance.

Original languageEnglish
Title of host publicationCollection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
Pages6684-6693
Number of pages10
Publication statusPublished - 2006
Event44th AIAA Aerospace Sciences Meeting 2006 - Reno, NV, United States
Duration: 2006 Jan 92006 Jan 12

Publication series

NameCollection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
Volume9

Other

Other44th AIAA Aerospace Sciences Meeting 2006
CountryUnited States
CityReno, NV
Period06-01-0906-01-12

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

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