Developing characteristics of subsonic-supersonic shear layers induced by different lobed mixers in the RBCC

J Li, C Ma, K Ma, Q Li - Acta Astronautica, 2023 - Elsevier
The rapid mixing of air and rocket gas is pivotal for enhancing combustion performance in
the ejector mode of rocket-based combined-cycle engines. This study experimentally …

Effect of Strut Schemes on Combustion Characteristics in Innovative Combined Ramjet Engine

K Zhang, F Qin, X Yu, S Zhu, D Zhang - Acta Astronautica, 2024 - Elsevier
The Mach 6-capable turbine based combined cycle engine is a potential first-stage
propulsion for TSTO mission. In order to improve thrust-to-weight ratio, an innovative tandem …

Investigation on sea-level thrust gain in ejector mode of rocket-based combined cycle engine

S Nie, F Qin, J Ye, X Wei, G He - Acta Astronautica, 2025 - Elsevier
One of the principal research subjects within the field of rocket-based combined cycle
(RBCC) engines has been the ejector mode, which has been the focus of research for a …

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

S Nie, G He, J Ye, X Wei, F Qin, S Zhu - Aerospace Science and …, 2024 - Elsevier
Variable geometry combustor technology is a novel technical approach for enhancing the
performance of rocket-based combined cycle (RBCC) engines. This research paper …

Thermal structure technology development of rocket based combined cycle engine

QIN Fei, Z Zheng, HE Guoqiang, J Tingting… - Acta Aeronautica et …, 2024 - sciopen.com
As one of the principal propulsion systems for the development of future horizontal take-off
and landing reusable earth-to-orbit transportation systems and near-space high-speed flight …