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  1. Effect of combustion chamber diameter size on scramjet rotating detonation under high Mach number flow conditions
  2. Influences of thermal physical property parameters on operating characteristics of simulated rotating detonation ramjet fueled by C12H23
  3. Numerical simulation of similarities between rotating detonation and high-frequency combustion instability under two mixing schemes
  4. Experimental investigation on effects of injection distribution on combustion instability in a model rocket combustor
  5. Structures of liquid jets in supersonic crossflows in a rectangular channel with an expansion section
  6. Propagation Mode Analysis on H2–Air Rotating Detonation Waves in a Hollow Combustor