Review on spray characteristics of liquid–liquid injectors in liquid rocket engines
Y Xie, J Zhang, M Sun, J Wu, P Li, B An, C Liang… - Physics of …, 2024 - pubs.aip.org
Impinging-jet injectors, liquid–liquid coaxial swirl injectors, and liquid–liquid pintle injectors
are representative liquid–liquid injectors in liquid rocket engines (LRE). For these liquid …
are representative liquid–liquid injectors in liquid rocket engines (LRE). For these liquid …
Dynamic flow behaviors of an inlet isolator in embedded rocket-driven mode transitions
X Yang, Z Tian, Y Yang, Y Yao, W Zhang, Z Wei… - Physics of …, 2024 - pubs.aip.org
The dynamic flow behaviors, as well as the propagation and coupling of regulation
information, in a rocket-based combined-cycle inlet isolator during the ejector-to-ramjet …
information, in a rocket-based combined-cycle inlet isolator during the ejector-to-ramjet …
Combustion organization strategies for a variable geometry RBCC combustor under low total temperature conditions
J Ye, Z Zhang, M Dai, S Nie, F Qin, X Wei - Applied Thermal Engineering, 2024 - Elsevier
A rocket-based combined cycle (RBCC) engine experiences a low Mach number phase
during flight operations. Through combustor geometry adjustment technology, the engine …
during flight operations. Through combustor geometry adjustment technology, the engine …
Numerical investigations on flow and heat transfer characteristics of a high-enthalpy double-cone in thermal and chemical non-equilibrium for hypersonic propulsion
C Dai, B Sun, D Zhao, S Zhou, C Zhou… - … Communications in Heat …, 2024 - Elsevier
There are strong interests in hypersonic propulsion communities in predicting the flow and
heat transfer characteristics over a hypersonic vehicle. However, this is quite challenging …
heat transfer characteristics over a hypersonic vehicle. However, this is quite challenging …
Combustion modes and oscillation characteristics in a rocket-dominated scramjet
Z Tian, G Zhao, X Zhang, A Fu, L Shi - Physics of Fluids, 2025 - pubs.aip.org
To investigate the combustion modes and the corresponding oscillation characteristics in
various operational states of a rocket-dominated scramjet, ground direct-connect …
various operational states of a rocket-dominated scramjet, ground direct-connect …
Research progress on mixing and combustion performance of strut/cavity-based combustor
Z Zijian, LIU Chaoyang, W HUANG - Acta Aeronautica et Astronautica …, 2024 - sciopen.com
Under hypersonic flight conditions, the residence time of fuel in the scramjet combustor is
extremely short, while sufficient mixing, ignition, and stable combustion of fuel and oxidants …
extremely short, while sufficient mixing, ignition, and stable combustion of fuel and oxidants …