Controlling the position of a stabilized detonation wave in a supersonic gas mixture flow in a plane channel

2017 ◽  
Vol 43 (3) ◽  
pp. 316-319 ◽  
Author(s):  
V. A. Levin ◽  
T. A. Zhuravskaya
Keyword(s):  
Detonation Wave ◽  
Plane Channel ◽  
Gas Mixture ◽  
Mixture Flow

Intelligent gas-mixture flow sensor

1995 ◽  
Vol 47 (1-3) ◽  
pp. 380-384 ◽  
Author(s):  
Theo S.J. Lammerink ◽  
Fred Dijkstra ◽  
Zweitze Houkes ◽  
Joost van Kuijk
Keyword(s):  
Flow Sensor ◽  
Gas Mixture ◽  
Mixture Flow

A Contribution to the Theory of the Development and Stability of Detonation in Gases

1952 ◽  
Vol 19 (1) ◽  
pp. 63-71
Author(s):  
A. K. Oppenheim
Keyword(s):  
Detonation Wave ◽  
Cross Section ◽  
Combustion Zone ◽  
Gas Mixture ◽  
Constant Cross Section ◽  
Combustion System ◽  
Adequate Explanation ◽  
System A

Abstract The development of detonation of an explosive gas mixture contained in a constant-cross-section duct is analyzed on the basis of a unidimensional, gasdynamic treatment of a double-discontinuity combustion system. A steady and an unsteady system are considered, and it is shown that the latter yields an adequate explanation of the effect of coalition of the two discontinuities on the establishment and subsequent stability of the detonation wave. The locus of states behind the detonating combustion zone during the development of the process is determined and analyzed.

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