Research progress on ejector mode of rocket-based combined-cycle engines
L Shi, G Zhao, Y Yang, D Gao, F Qin, X Wei… - Progress in Aerospace …, 2019 - Elsevier
Abstract The Rocket-based Combined-cycle (RBCC) engine is regarded as one of the most
efficient propulsion systems for reusable space transportation vehicles and hypersonic …
efficient propulsion systems for reusable space transportation vehicles and hypersonic …
Numerical analysis of flow features and operation characteristics of a rocket-based combined-cycle inlet in ejector mode
L Shi, X Liu, G He, F Qin, X Wei, B Yang, J Liu - Acta Astronautica, 2016 - Elsevier
A ready-made central strut-based rocket-based combined-cycle (RBCC) engine was
numerically investigated in the ejector mode. The flow features in the RBCC inlet and the …
numerically investigated in the ejector mode. The flow features in the RBCC inlet and the …
[HTML][HTML] Numerical investigation of cowl lip adjustments for a rocket-based combined-cycle inlet in takeoff regime
L Shi, X Liu, G He, F Qin, X Wei, B Yang… - International Journal of …, 2016 - degruyter.com
Numerical integration simulations were performed on a ready-made central strut-based
rocket-based combined-cycle (RBCC) engine operating in the ejector mode during the …
rocket-based combined-cycle (RBCC) engine operating in the ejector mode during the …
Dynamic Response of a Dual-Manifold Injector Rocket Engine to Throttling
P Cheng, Q Li, J Wu, Z Kang - Journal of Propulsion and Power, 2018 - arc.aiaa.org
The capability of a dual-manifold injector rocket engine scheme for deep throttling under
extremely fuel-rich condition was demonstrated experimentally. The dynamic response of …
extremely fuel-rich condition was demonstrated experimentally. The dynamic response of …