Numerical study on the induced-ramp mixed and combustion characteristics of rocket-based combined cycle engine-Reference-Cited by-同舟云学术

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Numerical study on the induced-ramp mixed and combustion characteristics of rocket-based combined cycle engine

Published:2021-11 Issue: Volume:118 Page:107068
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Jian Dai^ORCID,Chao Huang^ORCID,Fei Xu,Qiuru Zuo,Linyuan Peng

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference58 articles.

1. Survey on the mode transition technique in combined cycle propulsion systems;Huang;Aerosp. Sci. Technol.,2014

2. Artificial neural network based chemical mechanisms for computationally efficient modeling of hydrogen/carbon monoxide/kerosene combustion;An;Int. J. Hydrog. Energy,2020

3. Research progress on ejector mode of rocket-based combined-cycle engines;Shi;Prog. Aeronaut. Sci.,2019

4. An analysis tool of the rocket-based combined cycle engine and its application in the two-stage-to-orbit mission;Zhang;Energy,2020

5. Survey on key techniques of rocket-based combined-cycle engine in ejector mode;Dong;Acta Astronaut.,2019

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1. Numerical and experimental study of choking phenomenon on RBCC engines in ejector mode;Aerospace Science and Technology;2024-03

2. Experimental and numerical study on RBCC engines performance in simultaneous and combustion cycle;International Communications in Heat and Mass Transfer;2024-01

3. Numerical investigation on the combustion characteristics of powder fuel under different regulation parameters;Aerospace Science and Technology;2023-11

4. Spatiotemporal flow evolution in a rocket-based combined-cycle inlet during ejector-to-ramjet mode transition;Physics of Fluids;2023-10-01

5. Effect of passive strut angle on the vortical structures and mixing characteristics of scramjet combustor;Physics of Fluids;2023-06-01

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