Extension of the Laminar Flamelet Model to Account for Wall Heat Losses in Rocket Engine...

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Extension of the flamelet generated manifold approach to account for heat losses in multiphase combustor simulations

B Muralidharan, AC Zambon… - AIAA Propulsion and …, 2019 - arc.aiaa.org
This paper presents an extension to the Flamelet Generated Manifold (FGM) approach to
multiphase combustion. The two primary aspects of the extension of the FGM formulation to …
被引用次数：7 相关文章 所有 2 个版本

Flamelet/Progress Variable Formulation with Pressure Variations for Modeling Rocket Combustion Dynamics

A Hosangadi, AC Zambon, B Muralidharan… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
A zonal, multi-physics modeling framework for dynamic combustion processes, that can
capture relevant local physics and simulate system behavior while significantly reducing …
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Application of progress variable based tabulated chemistry approach to investigate spray combustion in gas turbine engines

B Muralidharan, AC Zambon… - AIAA Propulsion and …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-3636. vid This paper presents the
application of the multiphase non-adiabatic Multi-Time Scale Flamelet/Progress Variable …
被引用次数：1 相关文章

CRUNCH CFD® Turbulent Combustion Modeling Capabilities for Rocket Engine Applications

J Kim, H Jeon, S Kim, B Muralidhar… - 한국추진공학회학술 …, 2018 - dbpia.co.kr
This paper provides an overview of the implementation and validation of the Flamelet
Generated Manifold (FGM) combustion model into CRUNCH CFD®, CRAFT Tech's …
被引用次数：1 相关文章

RDE Diluent Mixing & Shock Negation

CA Nordeen, V Ahuja, SB Coogan - AIAA Scitech 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-0902. vid A co-annular diluent
injector and rotating detonation engine exhausts into a convergent conical annulus and …
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