Numerical study on the integration of three-dimensional n-decane/air rotating detonation combustor and supersonic turbine stage

Key Points

• Higher combustion efficiency is achieved with the rotating detonation combustor, coupled with the turbine stage.
• The combustion efficiency improved by 20% during the simulations involving n-decane and air.
• Numerical modeling focused on the integration of the three-dimensional rotating detonation combustor and the turbine stage.
• This integration may lead to significant advancements in turbine performance and efficiency.