Results 41 to 50 of about 4,282 (226)
At an extremely high Mach number, the regenerative cooling of traditional kerosene cannot meet the requirement of the heat sink caused by aerodynamic heating and internal combustion in a scramjet propulsion system.
Jian Liu +3 more
doaj +1 more source
Numerical Study on the Non-Oscillatory Unstarted Flow in a Scramjet Inlet-Isolator Model
For successful scramjet engine operations, it is important to understand the mechanism of the inlet unstart phenomenon. Among various unstarted flow patterns in hypersonic inlets, the mechanism of low-amplitude oscillatory unstarted flow is still unclear.
Jaewon Lee +3 more
doaj +1 more source
Modeling and analysis of regenerative cooling channels for scramjet engine [PDF]
This paper presents a CFD simulation analysis method for the regenerative cooling channel of a supercombustion ramjet engine, and performs three-dimensional modeling and analysis.
Gao Feng +4 more
doaj +1 more source
Abstract Novel compositionally complex borides, (Hf,Zr,Nb,Ti)B2 and (Hf,Zr,Nb,Ti)B2‒LaB6, were fabricated using spark plasma sintering process. (Hf,Zr,Nb,Ti)B2‒LaB6 exhibits a dual‐phase microstructure, in which (Hf,Zr,Nb,Ti)B2 is a primary phase with the hexagonal structure and LaB6 is a secondary phase with a cubic structure.
Xin Chen +8 more
wiley +1 more source
Performance comparison of full-scale ramjet and scramjet using boron-based propellant
This study investigates the performance boundaries of ramjet and scramjet engines fueled by boron-based propellant through full-scale engine modeling and three-dimensional computational fluid dynamics simulations.
Xianju Wu +5 more
doaj +1 more source
Experimental and numerical study of Richtmyer-Meshkov instability (RMI) induced mixing enhancement has been conducted in a liquid-fueled scramjet engine with a central strut.
Qingchun Yang, Juntao Chang, Wen Bao
doaj +1 more source
Numerical Study of Staged Transverse Injection of Sonic Jets into Supersonic Crossflows behind a Step [PDF]
Efficient combustion in the Scramjet combustors depends on the proper air-fuel mixing. Sufficient mixing between the supersonic airstream and the fuel jet is critical for designing of scramjet engines, and this is due to the very short residence ...
Mostafa Zahedzadeh, Fathollah Ommi
doaj +1 more source
Feasibility and Performance Analysis of High-Energy-Density Hydrocarbon-Fueled Turboexpander Engine
With the in-depth research on hypersonic aerodynamics and hypersonic propulsion technology, humans are growing closer to space travel. Recent studies have shown that the pre-cooled air-turborocket (ATR) or turboexpander engines are some of the potential ...
Jin Gao +5 more
doaj +1 more source
A high‐pressure shock‐tube facility is developed to investigate high‐temperature chemical‐kinetics for next‐generation combustion systems. The design enables extended test times and integrates multiple optical diagnostics for time‐resolved species detection.
Sulaiman A. Alturaifi +8 more
wiley +1 more source
Engine design heavily relies on numerical simulation of engine environments, which greatly accelerates the design iteration and increases efficiency. Nonetheless, for a long time, the uncertainty associated with numerical modeling has been overlooked due
Linying Li +4 more
doaj +1 more source

