Title of article :
Experimental Research on the Propagation Process of Continuous Rotating Detonation Wave
Author/Authors :
Zheng، نويسنده , , Quan and Weng، نويسنده , , Chun-sheng and Bai، نويسنده , , Qiao-dong، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2013
Pages :
7
From page :
201
To page :
207
Abstract :
In order to study the propagation mechanism of continuous rotating detonation wave, the H2/air continuous rotating detonation engine ignited by tangentially installed H2/O2 pre-detonation tube is studied experimentally using a tilt slot injector structure. The experimental results show that the stable rotating detonation wave can be gained successfully with the equivalent ratio of 0.93. The propagation frequency and velocity of rotating detonation wave range from 5200 to 5500 Hz and from 1518.5 to 1606.1 m/s, respectively. Three propagation modes, such as rotation, reversal and bifurcation, of detonation wave are verified through the analysis of propagation mechanism of rotating detonation wave.
Keywords :
Continuous rotating detonation engine , Experimental research , H2/air mixture , Slot injector , detonation wave
Journal title :
Defence Technology
Serial Year :
2013
Journal title :
Defence Technology
Record number :
2316875
Link To Document :
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