GAS PHASE IGNITION THEORY FOR HOMOGENEOUS PROPELLANTS UNDER SHOCK TUBE CONDITIONS

被引:12
作者
HERMANCE, CE
KUMAR, RK
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D O I
10.2514/3.5946
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:1551 / &
相关论文
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