A Preliminary Research on Combustion Characteristics of a Novel-Type Scramjet Combustor by Linqing Zhang, Juntao Chang, Wenxiang Cai, Hui Sun, Yingkun Li

“…The results indicate that the flow field and shock wave structure of such engine reveal similar characteristics as the classical DLR engine, and the variation in engine geometry can significantly affect its combustion characteristics. …”
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Reacting Flow Characteristics of Wall-mounted Ramps in Strut-injection Scramjet Combustors under Varying Hydrogen Jet Pressures by A. Antony Athithan, S. Jeyakumar

“…A rise in the hydrogen jet pressure accelerates flow downstream of the injector and reduces the intensity of shock wave interactions in ramp-based scramjet combustors. …”
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