Abstract
Let us consider again the one-dimensional gas flow with plane detonation wave having two-front structure (Fig. 1). The variations of velocity, pressure and density of the gas in each of the three regions, separated one of the other by adiabatic shock פ and heat release front f are described by equations of adiabatic gas flow (Pt. 1, Eqs (2.1)). Let the subscript ∞ denote the values ahead of adiabatic shock, the subscript 1 — the values inside the layer between two fronts, and let the values behind the heat release front be without any subscripts.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
Author information
Authors and Affiliations
Rights and permissions
Copyright information
© 1973 Springer-Verlag Wien
About this chapter
Cite this chapter
Cherny, G.G. (1973). Linear Stability Theory of Detonation Wave with Two-Front Structure. In: Lectures on the Theory of Exothermic Flows behind Shock Waves. International Centre for Mechanical Sciences, vol 36. Springer, Vienna. https://doi.org/10.1007/978-3-7091-2996-8_12
Download citation
DOI: https://doi.org/10.1007/978-3-7091-2996-8_12
Publisher Name: Springer, Vienna
Print ISBN: 978-3-211-81168-9
Online ISBN: 978-3-7091-2996-8
eBook Packages: Springer Book Archive