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

Journal article (2016)

Authors

F Diegelmann Technische Universität München
S. Hickel Aerodynamics - Aerospace Engineering , Technische Universität München
NA Adams Technische Universität München
Research Group
Aerodynamics (Aerospace Engineering) (TU Delft)
Copyright: © 2016 F Diegelmann, S. Hickel, NA Adams
DOI: https://doi.org/10.1016/j.combustflame.2016.09.014
More Info
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Published Date

2016

Language

English

Faculty

Aerospace Engineering

Department

Flow Physics and Technology

Research Group

Aerodynamics