z-logo
open-access-imgOpen Access
Reduced Order Modeling Approach to Combustion Instabilities of Liquid Rocket Engines
Author(s) -
Manuel Gonzalez-Flesca,
Philippe Scouflaire,
Thomas Schmitt,
Sébastien Ducruix,
Sébastien Candel,
Yoann Méry
Publication year - 2018
Publication title -
aiaa journal
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.828
H-Index - 158
eISSN - 1081-0102
pISSN - 0001-1452
DOI - 10.2514/1.j057098
Subject(s) - liquid propellant rocket , rocket (weapon) , combustion , rocket engine , mechanics , combustor , aerospace engineering , series (stratigraphy) , harmonic , physics , control theory (sociology) , engineering , computer science , acoustics , geology , propellant , chemistry , control (management) , organic chemistry , artificial intelligence , paleontology

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here
Accelerating Research

Address

John Eccles House
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom