Deflagration to detonation transition in large confined volume of lean hydrogen-air mixtures

被引:98
作者
Dorofeev, SB [1 ]
Sidorov, VP [1 ]
Dvoinishnikov, AE [1 ]
Breitung, W [1 ]
机构
[1] FORSCHUNGSZENTRUM KARLSRUHE, KARLSRUHE, GERMANY
关键词
D O I
10.1016/0010-2180(95)00113-1
中图分类号
O414.1 [热力学];
学科分类号
摘要
The results of large-scale experiments on turbulent flame propagation and transition to detonation in a confined volume of lean hydrogen-air mixtures are presented. The experiments were in a strong concrete enclosure of 480 m(3), and of 69.9 m length. The experimental volume consists first of a channel (34.6 m length, 2.3 m height, 2.5 m width) with or without obstacles, a canyon (10.55*6.3*2.5 m), and a final channel. Ignition was with a weak electric spark at the beginning of the first channel. The effect of hydrogen concentration (9.8%-14% vol.) on turbulent flame propagation and transition to detonation was studied. The obstacle configuration in the first channel (blockage ratio 0.3, 0.6, and no obstacles), exit cross section to the canyon (1.4, 2, and 5.6 m(2)), and vent area at the end (0, 2.5, and 4 m(2)) were varied in the tests. Details of turbulent flame propagation, of pressure field, and of detonation onset are presented. A minimum of 12.5% of hydrogen was found to be necessary for transition to detonation. This is a much less sensitive mixture than those in which the onset of spontaneous detonation has previously been observed (minimum of 15% of hydrogen in air). The effect of scale on the onset conditions for spontaneous detonation is discussed. The characteristic geometrical size of the mixture for transition to detonation is shown to be strongly related to the mixture sensitivity.
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页码:95 / 110
页数:16
相关论文
共 36 条
[1]   DEFLAGRATION DETONATION TRANSITION IN HYDROGEN AIR STEAM MIXTURES - RELEVANCE OF THE EXPERIMENTAL RESULTS FOR REAL ACCIDENT SITUATIONS [J].
BEHRENS, U ;
LANGER, G ;
STOCK, M ;
WIRKNERBOTT, I .
NUCLEAR ENGINEERING AND DESIGN, 1991, 130 (01) :43-50
[3]   TURBULENT JET INITIATION OF DETONATION [J].
CARNASCIALI, F ;
LEE, JHS ;
KNYSTAUTAS, R ;
FINESCHI, F .
COMBUSTION AND FLAME, 1991, 84 (1-2) :170-180
[4]  
CHAN CK, 1988, 22 S INT COMB COMB I, P1733
[5]  
Desbordes D., 1993, Progress in Astronautics and Aeronautics, V153, P347, DOI DOI 10.2514/5.9781600866265.0347.0359
[6]   EVALUATION OF THE HYDROGEN EXPLOSION HAZARD [J].
DOROFEEV, SB ;
KOCHURKO, AS ;
EFIMENKO, A ;
CHAIVANOV, BB .
NUCLEAR ENGINEERING AND DESIGN, 1994, 148 (2-3) :305-316
[7]  
DOROFEEV SB, 1991, IRIS912 SR DO IND RI
[8]  
DOROFEEV SB, 1993, RRCKI8005 RRC KURCH
[9]  
DOROFEEV SB, 1993, 14TH INT C DYN EXPL, V2
[10]  
DOROFEEV SB, 1989, 16TH S INT LOSS PREV, V4