The response of a nominally two-dimensional transonic diffuser flow to abrupt downstream perturbations was examined experimentally.
Terminal Shock Response in Ramjet Inlets to Abrupt Downstream Perturbations
1988
47 pages
Report
No indication
English
Jet & Gas Turbine Engines , Combustion & Ignition , Fluid Mechanics , Ramjet engines , Ramjet inlets , Downstream flow , Perturbations , Transonic flow , Response , Shock waves , Diffusers , Combustion stability , Pressure , Oscillation , Acoustic waves , Elastic waves , Interactions , Transonic diffusers , Combustion instability , Convective waves , Terminal shock waves
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