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Pulse-detonation study by diagnostic optical techniques

Abstract

Pulse detonation engines (PDE) have been recently recognized as new propulsion technology devices, which have potential application to the subsonic, supersonic and hypersonic flight regime. There are several applications for this devices, the most promising is related to the hypersonic scramjet (supersonic combustion ram jet) engine development. In this work, a pulse detonation system with similar features as PDE will be build. The aim is the study of the detonation process through diagnostic techniques. At first, the experimental conditions next to those at flight Mach number lower or equal to 6 will be investigated. The methodologies time-resolved spectroscopic emission measurements from OH* and H2O* species with vibrational resolution and pressure changes as function of detonation front propagation and detonation wave expansion in the test chamber will be employed. Hence, it will be possible to characterize and evaluate the pulse detonation system in the study conditions allowing establish correlations with engines in supersonic to hypersonic flight regime. (AU)

Articles published in Agência FAPESP Newsletter about the research grant:
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VEICULO: TITULO (DATA)
VEICULO: TITULO (DATA)

Scientific publications
(References retrieved automatically from Web of Science and SciELO through information on FAPESP grants and their corresponding numbers as mentioned in the publications by the authors)
LOPES, NATHAN C.; KATATA, CARLOS C. B.; MARQUES, CARLA S. T.. Diagnostic method based on spontaneous emission to evaluate the detonation cycle. EXPERIMENTAL THERMAL AND FLUID SCIENCE, v. 102, p. 261-270, . (08/10548-5)