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

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

研究成果: Conference contribution

摘要

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.

原文English
主出版物標題Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
頁面6684-6693
頁數10
出版狀態Published - 2006
事件44th AIAA Aerospace Sciences Meeting 2006 - Reno, NV, United States
持續時間: 2006 1月 92006 1月 12

出版系列

名字Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
9

Other

Other44th AIAA Aerospace Sciences Meeting 2006
國家/地區United States
城市Reno, NV
期間06-01-0906-01-12

All Science Journal Classification (ASJC) codes

  • 空間與行星科學
  • 航空工程

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