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This paper discusses experimental research on the aerodynamic characteristics of base bleeding with combustion of fuel-rich solid fuel in flows at subsonic, transonic, and supersonic speeds. The effects of ejection parameter, freestream Mach number, geometry parameter of jet hole, rotary speed of model, and combustion temperature at jet hole on the base drag reduction rate for the model are investigated. The results show significant differences of drag reduction characteristics between base combustion of fuel-rich solid fuel and base bleeding of cold or hot gas.
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Ding et al. (1992) studied this question.
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