Simulation and application of a new multiphase flow ablation test system for thermal protection materials based on liquid rocket engine
Q Su, B Zha, J Wang, M Yan, Y Gao, Z Sun, W Huang - Aerospace, 2022 - mdpi.com
Internal flow field ablation is an important issue in thermal protection materials for rocket
engines and hypersonic vehicles. In this paper, a new multiphase flow ablation test system …
engines and hypersonic vehicles. In this paper, a new multiphase flow ablation test system …
Analyzing combustion efficiency according to spray characteristics of gas-centered swirl-coaxial injector
S Woo, J Lee, I Lee, S Kim, Y Han, Y Yoon - Aerospace, 2023 - mdpi.com
The momentum flux ratio (MFR) significantly affects the mixing characteristics and
combustion efficiency of propellants in rocket engine injectors. The spray characteristics of …
combustion efficiency of propellants in rocket engine injectors. The spray characteristics of …
Oxidation Behavior of Atmospheric Plasma Sprayed NiAl Coating at High Pressure Oxygen Atmosphere
L Zhang, XJ Liao, XT Luo, CJ Li - Materials Science Forum, 2023 - Trans Tech Publ
The high-temperature and high-pressure oxygen-rich combustion gases often cause the
high temperature gas conduit in rocket engine to suffer severe oxidation, resulting in a …
high temperature gas conduit in rocket engine to suffer severe oxidation, resulting in a …