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home > research > past major research > supersonic base flow

about LES/RANS hybrid methodology
current research focus
past major research
computational study of a supersonic base flow with LES/RANS hybrid methodology
analysis and prediction of thin-airfoil stall phenomena with LES/RANS hybrid methodology
numerical analysis of pulse detonation engine cycles

background: engineering background & motivation


Supersonic flows past an axisymmetric base are fundamental but important for many engineering problems, such as a rocket, re-entry capsule, aerospike nozzle, reusable launch vehicle, etc. The pressure that establishes itself at the base of a projectile, whether powered or not, is almost always noticeably lower than that of the free-stream.
reusable launch vehicle at JAXA/ISAS.
This pressure which is determined by the flow field behind the base causes significant base drag, and the aerodynamics performances of these vehicles are considerably influenced. Unsteady pressure fluctuation at the base sometimes loses dynamic stability of a vehicle. Therefore, accurate estimations of base flows and a resulting force acting on the base are important issues for many engineering problems, such as for the design of these vehicles. Furthermore, the knowledge of base flows lies in the ability to control the near wake flow interactions such that base drag can be reduced and vehicle stability and control can be enhanced.
   
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