Título:	Theoretical and experimental study of combustion instability in hybrid rocket motors
Autor(es):	Bertoldi, Artur Elias de Morais Bouziane, Mohammed Lee, Jungpyo Veras, Carlos Alberto Gurgel Hendrick, Patrick Simone, Domenico
Assunto:	Motores de foguetes Câmaras de combustão
Data de publicação:	2019
Editora:	EUCASS association
Referência:	BERTOLDI, Artur Elias de Morais et al. Theoretical and experimental study of combustion instability in hybrid rocket motors. In: EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), 8., 2019, Madri. Proceedings [...]. Madrid: EUCASS association, 2019. DOI: 10.13009/EUCASS2019-538. Disponível em: https://www.eucass.eu/index.php/conferences-and-publications/search-in-publications?searchword=eucass/2019&searchphrase=all&limit=20&areas[0]=doc_indexer&start=280. Acesso em: 02 dez. 2019.
Abstract:	This work describes a theoretical and experimental study of combustion instability in hybrid rocket motors. Results are highlighting that the parameter Δ𝑝 /𝑝̅c (pressure drop between tank and chamber scaled by average chamber pressure) plays an important role in the oscillatory characteristics of the chamber pressure. By modifying the feed-system-coupled instability theory, a combustion time lag model has been developed; using this a new general analysis criterion is proposed. Results show good agreement with the experimental data and suggest that the combustion time delay of the liquid oxidizer is more important than the response time of solid fuel boundary layer.
Unidade Acadêmica:	Faculdade de Ciências e Tecnologias em Engenharia (FCTE) – Campus UnB Gama
DOI:	10.13009/EUCASS2019-538
Versão da editora:	https://www.eucass.eu/index.php/conferences-and-publications/search-in-publications?searchword=eucass/2019&searchphrase=all&limit=20&areas[0]=doc_indexer&start=280
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