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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

PDE: about detonation and PDE


A detonation phenomenon is the interaction between a front-running shock wave and subsequent coupled combustion, generating a high pressure and temperature which is basically uncontrollable in comparison with conventional flames. The direction of research has mostly been prevention of or protection from hazard.
For several years , however, there has been a trend to control detonation propagation, and to utilize its high power and high-density energy in positive directions like pulse detonation engine (PDE).
PDRE of ASI: Aviation Week and Space Technology, July 2000.
PDE represents a concept which has the potential of providing improvements in the ratio of performance to price over conventional air breathing propulsion devices. The operational principle of PDE can be explained briefly in the following. As a simplest example, a rocket-engine-type PDE operation of cylindrical shape is considered. The cycle operation of PDE consists of the three phases which are combustion, exhaustion and fuel supply. A mixture of hydrogen fuel and oxygen is supplied into PDE, followed by the ignition of mixture by an igniter placed over the closed upstream end. The combustion wave is acelerated to a detonation and propagates downstream in PDE. Thereafter, the detonation wave is emitted from PDE exit, with the burnt gas being exhausted. By repeating such four phases, PDE generates thrust.
   
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