The combustion process in rocket-assisted subsonic ramjet engines represents a key
advancement in integrated aerospace propulsion, particularly for embedded rocket-based …

The combustor is the core component of the scramjet. The mixing of fuel and oxidizer is an
important prerequisite for the efficient operation of the combustor. A thin strut configuration …

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 …

A rocket-based combined cycle (RBCC) engine experiences a low Mach number phase
during flight operations. Through combustor geometry adjustment technology, the engine …

To understand the actual operation of detonation engines, it is of great significance to
simulate the detonation characteristics after being affected by unsteady supersonic flow …

To investigate the combustion modes and the corresponding oscillation characteristics in
various operational states of a rocket-dominated scramjet, ground direct-connect …

The search for optimal methods of interaction with supersonic flows using blown gas jets is
an important and relevant area that is currently receiving great attention. In this paper, a …

로켓 기반 복합추진시스템 (RBCC, Rocket Based Combined Cycle) 은 넓은 비행 영역과
마하수에서 비행이 가능한 엔진으로 엔진 내부에 장착된 소형 로켓을 이용한 이젝션 효과로 …