Experimental investigation on performance variation and dynamic characteristics of a variable geometry rocket-based combined cycle combustor-Reference-Cited by-同舟云学术

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Experimental investigation on performance variation and dynamic characteristics of a variable geometry rocket-based combined cycle combustor

Published:2024-10 Issue: Volume:153 Page:109442
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Nie Shao,He Guoqiang,Ye Jinying^ORCID,Wei Xianggeng^ORCID,Qin Fei,Zhu Shaohua

Funder

Natural Science Basic Research Program of Shaanxi Province

Publisher

Elsevier BV

Reference24 articles.

1. Rocket-based combined cycle propulsion technology for access-to-space applications;Hueter,1999

2. The Role of the Strutjet Engine in New Global and Space Markets;Siebenhaar,1998

3. Research Progress of Rocket Based Combined Cycle Engines;Wang;Jounal of Astronautics,2019

4. Experimental study on ejector-to-ramjet mode transition in a divergent kerosene-fueled RBCC combustor with low total temperature inflow;Shi;Aerosp. Sci. Technol.,2020

5. Experimental study on combustion modes of a liquid kerosene fueled RBCC combustor;Xue;Fuel,2017

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