Reduced-order modeling of supersonic fuel–air mixing in a multi-strut injection scramjet engine using machine learning techniques-Reference-Cited by-同舟云学术

Reduced-order modeling of supersonic fuel–air mixing in a multi-strut injection scramjet engine using machine learning techniques

Published:2023-01 Issue: Volume:202 Page:564-584
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ispir Ali C.^ORCID,Zdybał Kamila^ORCID,Saracoglu Bayindir H.^ORCID,Magin Thierry,Parente Alessandro,Coussement Axel

Funder

Horizon 2020 Framework Programme

Horizon 2020

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference59 articles.

1. Estimation of vitiation effects on flameholding and mode transition in a dual-mode supersonic combustor;Wu;Acta Astronaut.,2021

2. Numerical exploration of mixing and combustion in a dual-mode combustor with backward-facing steps;Huang;Acta Astronaut.,2016

3. Combustion of hydrogen in hot air flows within LAPCAT-II Dual Mode Ramjet combustor at Onera-LAERTE facility-experimental and numerical investigation;Vincent-Randonnier,2014

4. Mixing characteristics of inclined fuel injection via various geometries for upstream-fuel-injected scramjets;Ogawa;J. Propuls. Power,2015

5. Scramjets: Fuel Mixing and Injection Systems;Gerdroodbary,2020

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