Characteristics of flame acceleration and deflagration-to-detonation transition enhanced by SF6 jet-in-cross-flow/flame interaction-Reference-Cited by-同舟云学术

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Characteristics of flame acceleration and deflagration-to-detonation transition enhanced by SF6 jet-in-cross-flow/flame interaction

Published:2023-09 Issue: Volume:140 Page:108451
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cheng Jun,Zhang Bo^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference46 articles.

1. Stabilized detonation for hypersonic propulsion;Rosato;Proc. Natl. Acad. Sci.,2021

2. Overview of performance, application, and analysis of rotating detonation engine technologies;Rankin;J. Propuls. Power,2017

3. Review on the research progresses in rotating detonation engine;Nejaamtheen,2018

4. Performance analysis of dual-duct rotating detonation aero-turbine engine;Ji;Aerosp. Sci. Technol.,2019

5. Propulsion performance of cylindrical rotating detonation engine;Yokoo;AIAA J.,2020

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2. Investigation on Accelerated Initiation of Oblique Detonation Wave Induced by Laser-Heating Hot-Spot;Aerospace;2024-06-19

3. Enhancing detonation propulsion with jet in cross-flow: A comprehensive review;Progress in Aerospace Sciences;2024-05

4. Dynamic Measurement and Prediction of Sulfur Hexafluoride Gas Weight Based on Non-Ideal Gas State Equation and Improved Random Forest;Journal of Nanoelectronics and Optoelectronics;2024-04-01

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