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Effect of Mach number on the mode transition for supersonic cavity flows

Chao Zhang, Renfu Li, Zhaojun Xi, Zhen‐Hua Wan, De‐Jun Sun

2020Aerospace Science and Technology16 citationsDOI

Topics & Concepts

Dynamic mode decompositionMach numberSupersonic speedBoundary layerMechanicsOscillation (cell signaling)VortexMode (computer interface)WakePhysicsChoked flowEquilibrium mode distributionInstabilityFlow (mathematics)Mach waveBoundary layer thicknessDynamic pressureOpticsSingle-mode optical fiberRadiation modeGeneticsComputer scienceBiologyLaserOperating systemAerodynamics and Acoustics in Jet FlowsFluid Dynamics and Turbulent FlowsFluid Dynamics and Vibration Analysis
Effect of Mach number on the mode transition for supersonic cavity flows | Litcius