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 …
propulsion for TSTO mission. In order to improve thrust-to-weight ratio, an innovative tandem …
Dynamic characteristic comparison between pressure fluctuations coupling with a moving part model of a liquid rocket engine flow regulator
P Jin, X Shang, G Cai - Physics of Fluids, 2024 - pubs.aip.org
The rapid development of space launch vehicle has put forward increasingly strict
requirements for engine startup characteristics and thrust regulation capabilities. The flow …
requirements for engine startup characteristics and thrust regulation capabilities. The flow …
Unsteady separation mechanism of ground horizontal-sliding takeoff system
H Qian, W Wang, Y Jiang, P Yan, Y Cai - Physics of Fluids, 2024 - pubs.aip.org
Complex aerodynamic interference has long posed challenges to the safe separation of
multi-body systems. Based on a new conceptual ground horizontal-sliding takeoff approach …
multi-body systems. Based on a new conceptual ground horizontal-sliding takeoff approach …