This viewgraph representation provides an overview of research which develops a quasi one dimensional chemistry computational fluid dynamics code to study the effect of nozzle design on the performance of pulse detonation rocket engines (PDREs). Topics considered include: PDREs vs. steady-state rocket engines (SSREs), PDRE cycles, numerical models of idealized PDRE performance, thrust determination of PDRE, specific geometries, and nozzle design and geometry.
Quasi 1-D Study of Pulse Detonation Rocket Engine Blowdown Gasdynamics and Performance
Propulsion Engineering Research Center 14th Annual Symposium on Propulsion ; 2002 ; State College, PA, United States
02.12.2002
Preprint
Keine Angabe
Englisch
Simplified Analysis of Pulse Detonation Rocket Engine Blowdown Gasdynamics and Performance
British Library Conference Proceedings | 2002
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