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Chin. Phys. B, 2012, Vol. 21(12): 124702    DOI: 10.1088/1674-1056/21/12/124702
ELECTROMAGNETISM, OPTICS, ACOUSTICS, HEAT TRANSFER, CLASSICAL MECHANICS, AND FLUID DYNAMICS Prev   Next  

Experimental investigations of detonation initiation by hot jets in supersonic premixed flows

Han Xu (韩旭), Zhou Jin (周进), Lin Zhi-Yong (林志勇)
Science and Technology on Scramjet Laboratory, National University of Defence Technology, Changsha 410073, China
Abstract  A new method to initiate and sustain the detonation in supersonic flow is investigated. The reaction activity of coming flow may influence the result of detonation initiation. When a hot jet initiates a detonation wave successfully, there may exist two types of detonations. If the detonation velocity is greater than the velocity of coming flow, there will be a normal detonation here. Because of the influence of boundary layer separation, the upstream detonation velocity is much greater than the Chapman-Jouguet (CJ) detonation velocity. On the other hand, if the detonation velocity is less than the velocity of coming flow, an oblique detonation wave (ODW) will form. The ODW needs a continuous hot jet to sustain itself. If the pressure of jet is lower than a certain value, the ODW will decouple. In contrast the normal detonation wave can sustain itself without the hot jet.
Keywords:  hot jet      detonation      supersonic flow  
Received:  12 March 2012      Revised:  08 June 2012      Accepted manuscript online: 
PACS:  47.40.Rs (Detonation waves)  
  47.40.Ki (Supersonic and hypersonic flows)  
  47.40.-x (Compressible flows; shock waves)  
Fund: Project supported by the National Natural Science Foundation of China (Grant Nos. 91016028 and 91016012).
Corresponding Authors:  Han Xu     E-mail:  hanxuyun@yahoo.com.cn;zj706@vip.sina.com

Cite this article: 

Han Xu (韩旭), Zhou Jin (周进), Lin Zhi-Yong (林志勇) Experimental investigations of detonation initiation by hot jets in supersonic premixed flows 2012 Chin. Phys. B 21 124702

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