IGNITION OF HOMOGENEOUS SOLID PROPELLANTS UNDER SHOCK TUBE CONDITIONS - FURTHER THEORETICAL DEVELOPMENT

被引:6
作者
KUMAR, RK
HERMANCE, CE
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D O I
10.2514/3.49964
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:1615 / &
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