Summary
A deflagration wave was generated by putting a perforated plate in the way of a self-sustained detonation wave and interrupting it. We investigated the averaged one dimensional structure of this deflagration wave and its development through streak schlieren photography and wave speed measurement. With the increase of initial pressure, the deflagration wave varies from a laminar structure to a turbulent one. The former usually can not stand the attenuation of background rarefaction, whereas the later is capable of running up followed by an abrupt transition to detonation waves. There is a very unstable critical case between above-mentioned two situations, where the deflagration wave can usually propagate for a relatively long distance in 50-60 % CJ detonation speed. Theoretical analysis also reveals that the state of its products in this critical case perfectly matches the constant-volume combustion solution in same mixture.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
J.H.S. Lee, On the Transition from Deflagration to Detonation, of Progress in Astronautics and Aeronautics series, 1986, Vol.106, pp.644
G.Dupre, O.Peraldi, J.H.S.Lee, et al. Propagation of Detonation Waves in an Acoustic Absorbing Walled Tube, Progress in Astronautics and Aeronautics, 1988, Vol.114, pp.248-263
A. Teodorcyzk, and J.H.S.Lee, Detonation Attenuation by Foams and Wire Meshes Lining the Walls, Shock Waves (1995), Vol.4, pp.225-236
M.I.Radulescu and J.H.S.Lee, The Failure Mechanism of Gaseous Detonations: Experiments in Porous Wall Tubes, Combustion and Flame, 2002, 131:29-46
C. Guo, G. Thomas, J. Li and D. Zhang, et al, Experimental Study of Gaseous Detonation Propagation over Acoustically Absorbing Walls, Shock Waves (2002), 11: 353-359
R.S. Chue, J. H. Lee, T. Scarinci, et al. Transition from Fast Deflagration to Detonation Under the Influence of Wall Obstacles, Progress in Astronautics and Aeronautics, 1992, Vol.153
G.O.Thomas, R.J.Bambrey, and C,Brawn, Experimental observations of flame acceleration an transition to detonation following shock-flame interaction. Combust. Theory Modelling, 5(2001)573-594
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2009 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Zhu, Y., Liang, Z., Lee, J., Yang, J. (2009). Study on perforated plate induced deflagration waves in a smooth tube. In: Hannemann, K., Seiler, F. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-85168-4_62
Download citation
DOI: https://doi.org/10.1007/978-3-540-85168-4_62
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-85167-7
Online ISBN: 978-3-540-85168-4
eBook Packages: EngineeringEngineering (R0)