Publication | Closed Access
Bow shock/jet interaction in compressible transverse injection flowfields
82
Citations
11
References
1996
Year
AeroacousticsUnsteady FlowCompressible FlowEngineeringAerospace EngineeringSupersonic CombustionFluid MechanicsFlow PhysicTurbulence ModelingTurbulent Flow Heat TransferAerodynamicsDominant FeaturesPropulsionSeparation ShocksMultiphase FlowTransverse InjectionShock CompressionBow Shock/jet Interaction
In flowfields created by transverse injection into supersonic cross-flows, the bow and separation shocks formed upstream of the injectant plume are dominant features. In the present investigation, the interaction between these features and the large-scale eddies that develop at the jet/freestream interface has been examined.
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