Improvement of Mixing Efficiency in the Combustion Chamber of a Powder-Fuel Ramjet Engine
Frontiers in Energy Research, 2021 The challenge of the powder-fuel ramjet is to improve the mixing effect of powder-fuel with oxidizing agents and combustion efficiency. To improve the mixing and combustion efficiency of the powder-fuel ramjet engine, three configurations in head shapes ...
Wenxiong Xi, Jian Liu, Ren Mengfei
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Intensification of heat-exchange of a direct-flow steam boiler of a coil type based on an educational laboratory stand [PDF]
E3S Web of Conferences, 2023 In the work under consideration, using an experimental stand formed by a cylindrical coil, the modes of air movement through the flue of a ramjet steam boiler were investigated. Experimental studies have revealed shortcomings in the operation of a direct-
Bekhterev Dmitriy +4 more
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Design Method and Characteristics of an Inward-Turning Inlet Combining ICFA with Pressure Gradient
气体物理The performance of the inward-turning inlet is mainly determined by the axisymmetric basic flowfield. Using the ICFA (internal conical flow A) flowfield outlet as the initial boundary and specifying the pressure gradient distribution along the ...
Xiong GAO +4 more
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Pseudo-shock waves and their interactions in high-speed intakes [PDF]
, 2016 In an air-breathing engine the flow deceleration from supersonic to subsonic conditions takes places inside the isolator through a gradual compression consisting of a series of shock waves.
Gnani, F., Kontis, K., Zare-Behtash, H.
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Equation of motion of an interstellar Bussard ramjet with radiation and mass losses
, 2007 An interstellar Bussard ramjet is a spaceship using the protons of the interstellar medium in a fusion engine to produce thrust. In recent papers, it was shown that the relativistic equation of motion of an ideal ramjet and of a ramjet with radiation ...
Abramowitz +11 more
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A method for comparing the performance of power plants for vertical flight [PDF]
, 1952 A new method of power plant selection for vertical flight is proposed. It can be used to determine whether the performance of a rocket design can be improved by substituting for the rocket motor a different power plant such as a ramjet.
Tsien, H. S.
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C/C-SiC Composites for Nozzle of Solid Propellant Ramjet
Journal of Aeronautical Materials, 2017 Carbon fiber reinforced carbon and silicon carbide matrix composites for nozzle inner of solid propellant ramjet were prepared by using the hybrid process of "chemical vapor infiltration + precursor impregnation pyrolysis (CVI+PIP)".
WANG Lingling +5 more
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An Experimental Study of the Performance of a Subscale Kerosene - Fuelled Ejector Ramjet at Simulated Takeoff [PDF]
, 1996 The ejector ramjet is a rocket based combined cycle propulsion system in which a rocket and ramjet are integrated to accrue synergistic benefits. A proof-of-concept experiment to augment the thrust of a simulated rocket by the induction of air through ...
Isaac, JJ +7 more
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International Journal of Aerospace Engineering, Volume 2026, Issue 1, 2026.The increasing atmospheric carbon dioxide (CO2) concentration represents a major challenge in climate change mitigation. Carbon capture and storage (CCS) technology has emerged as an effective solution for CO2 emissions reduction, where the compression process plays a crucial role due to its significant energy requirements.
Mostafa Zahedzadeh +3 more
wiley +1 more source
Thermal Release Characteristics of Aeroengine Combustor Outlet Modulated by Gliding Arc Plasma
Advanced Science, Volume 12, Issue 41, November 6, 2025.Gliding arc plasma‐assisted combustion significantly improves aeroengine combustor. Gliding arc plasma moves flames closer to the fuel source, enabling complete burning. This increases the combustion efficiency by 10.3% and raises outlet temperature by 141.6°C.
Lei Zhang +5 more
wiley +1 more source