A Mathematical and Numerical Model for the Analysis of Hybrid Rocket Motors

A Mathematical and Numerical Model for the Analysis of Hybrid Rocket Motors

The hybrid rocket motors (HRM) use a two-phase propellant system. This offers some remarkable advantages but also arises some difficulties like the neutralization of their instabilities. The non-acoustic combustion instabilities are high-amplitude pressure oscillations that have too low frequencies...

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Bibliographic Details
Main Authors: Florin MINGIREANU, Marius STOIA-DJESKA
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2011-12-01
Series:INCAS Bulletin
Subjects:
hybrid combustion process
hybrid rocket motors
non-linear hyperbolic system
Online Access:http://bulletin.incas.ro/files/stoia_mingireanu_v3_iss_4_full.pdf

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