Shock Mach number influence on reaction wave types and mixing in reactive shock–bubble interaction

Journal Article (2016)
Author(s)

F Diegelmann (Technische Universität München)

S. Hickel (TU Delft - Aerodynamics, Technische Universität München)

NA Adams (Technische Universität München)

Research Group
Aerodynamics
Copyright
© 2016 F Diegelmann, S. Hickel, NA Adams
DOI related publication
https://doi.org/10.1016/j.combustflame.2016.09.014
More Info
expand_more
Publication Year
2016
Language
English
Copyright
© 2016 F Diegelmann, S. Hickel, NA Adams
Research Group
Aerodynamics
Volume number
174
Pages (from-to)
85-99
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.