Dual combustor ramjet engine dynamics modeling and simulation for design analysis

An integrated low-order, medium-fidelity model for a dual combustor ramjet engine configuration is derived for use in mission analysis and controller design. Each of the individual components – intake, isolator, ram diffuser and combustor, scram combustor and nozzle – are modeled using either empiri...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2019-03, Vol.233 (4), p.1307-1322
Hauptverfasser:	Wadwankar, N, Kandasamy, G, Ananthkrishnan, N, Renganathan, VS, Park, Ik-Soo, Hwang, Ki-Young
Format:	Artikel
Sprache:	eng
Schlagworte:	Combustion chambers Computer simulation Configurations Control systems design Control theory Design analysis Diffusers Dynamic stability Empirical analysis Feedback loops Nozzles Ramjet engines Throttling
Online-Zugang:	Volltext
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