Analysis of mild ignition in a shock tube using a highly resolved 3D-LES and high-order shock-capturing schemes
Author:
Funder
DFG
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-018-0867-4.pdf
Reference41 articles.
1. Mirels, H.: Attenuation in a shock tube due to unsteady-boundary-layer action. NACA-TR-1333, National Advisory Committee for Aeronautics (1957)
2. White, D.R.: Influence of diaphragm opening time on shock-tube flows. J. Fluid Mech. 4(6), 585–599 (1958). https://doi.org/10.1017/s0022112058000677
3. Petersen, E.L., Hanson, R.K.: Nonideal effects behind reflected shock waves in a high-pressure shock tube. Shock Waves 10(6), 405–420 (2001). https://doi.org/10.1007/pl00004051
4. Meyer, J.W., Oppenheim, A.K.: On the shock-induced ignition of explosive gases. Proc. Combust. Inst. 13(1), 1153–1164 (1971). https://doi.org/10.1016/s0082-0784(71)80112-1
5. Blumenthal, R., Fieweger, K., Komp, K.H., Adomeit, G.: Gas dynamic features of self ignition of non diluted fuel/air mixtures at high pressure. Combust. Sci. Technol. 123(1–6), 1–30 (1997). https://doi.org/10.1080/00102209708935637
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