The flowfields associated with truncated annular plug nozzles of varying lengths are studied both experimentally and using computational tools. The nozzles are designed to observe wake structure transition for the range of pressure ratios considered. A classification of the open wake regime is proposed for comparing and analyzing the plug flowfields. The three-dimensional relief experienced by the annular plug flow leads to greater wave interactions on the plug surface as compared with linear plug flow, resulting in a delayed transition of the base wake. The Reynolds averaged Navier–Stokes based solvers employed in the studies could predict the plug surface flow accurately, whereas they exhibited limitations with regard to plug base flow predictions. Based on the experimental data generated, an empirical model for predicting closed wake base pressure is proposed and compared with other models available in literature.
Analysis of Annular Plug Nozzle Flowfield
Journal of Spacecraft and Rockets ; 51 , 2 ; 478-490
2014-02-20
13 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Analysis of Annular Plug Nozzle Flowfield
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