Reduced-order modeling for non-equilibrium air flows

Alessandro Munafò, Simone Venturi, Maitreyee P. Sharma, Marco Panesi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This work deals with the development and application of reduced-order models for nonequilibrium hypersonic air flows. Starting from a State-to-State formulation, the reduction of kinetics mechanism to a more tractable form for Computational-Fluid-Dynamics (CFD) applications is realized by grouping the atom/molecule internal states within bins with prescribed population distributions. The group/bin-averaged kinetic parameters (e.g., rate coefficients) are computed in conjunction with Quasi-Classical-Trajectory (QCT) calculations. This allows for treating diatom-diatom systems (e.g., N2-N2) for which a State-to-State method is simply impractical. The proposed physico-chemical models are first compared against State-to-State formulations in zero and one-dimensional configurations to assess their accuracy, and later applied to realistic multi-dimensional simulations to demonstrate their maturity and predictive capabilities.

Original languageEnglish (US)
Title of host publicationAIAA Scitech 2020 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105951
DOIs
StatePublished - 2020
EventAIAA Scitech Forum, 2020 - Orlando, United States
Duration: Jan 6 2020Jan 10 2020

Publication series

NameAIAA Scitech 2020 Forum
Volume1 PartF

Conference

ConferenceAIAA Scitech Forum, 2020
Country/TerritoryUnited States
CityOrlando
Period1/6/201/10/20

ASJC Scopus subject areas

  • Aerospace Engineering

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