| Citation: | Zhao Qianpeng, Zhu Shaohua, Qin Yunpeng, et al. Direct-connection experimental investigation of an oblique detonation combustor with kerosene fuel internal injection[J]. Journal of Aerospace Power, 2026, 41（9）：20240808 doi: 10.13224/j.cnki.jasp.20240808
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In order to investigate the combustion mechanism of oblique detonation with hydrocarbon fuel internal injection, numerical simulations and direct-connected combustion heating experiments were conducted on an oblique detonation combustor simulating a flight Mach number of 8. A small-scale oblique detonation experimental piece was designed and the aviation kerosene was used as the fuel. Fuel injection and atomization was organized through 4×
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