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Kühlsystem
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Research progress on active thermal protection for hypersonic vehicles
Parametric performance analysis of multiple re-cooled cycle for hydrogen fueled scramjet
Performance cycle analysis of an open cooling cycle for a scramjet
Effects of wall cooling on performance parameters of hypersonic inlets
Interaction mechanism between shock waves and supersonic film cooling with cracking reaction
Quasi-One-Dimensional Model of Scramjet Combustor Coupled with Regenerative Cooling
Comparison During a Scramjet Regenerative Cooling and Recooling Cycle