Analysis of combustion modes in a cavity based scramjet
Combustion and Flame, 2020 Large eddy simulations (LES) of non reactive and reactive flows in a cavity-based scramjet combustor configuration from the U.S Air Force Research Laboratory (AFRL) are performed.
J. Ruan, P. Domingo, G. Ribert
semanticscholar +1 more source
Development of the fuel heating device for the component test of aerospace propulsion systems
Journal of Fluid Science and Technology, 2016 For the next generation space launch vehicle, fully reusable spaceplane with rocket and ramjet combined propulsion system is proposed. That type of spaceplane can drastically reduce the cost per unit mass of the payload.
Mitsuhiro SOEJIMA +3 more
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, 2020 Understanding start–unstart behavior of intakes in hypersonic Mach numbers is essential for seamless operation of scramjet engines.
M. K. Devaraj +4 more
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CFD Investigation of Supersonic Scramjet Exhaust Geometry for Emission Reduction and Sustainable Hypersonic Propulsion [PDF]
EPJ Web of ConferencesThis study employs CFD analysis to optimize the scramjet exhaust divergent angle with the aim of improving propulsion efficiency and reducing environmental impact in hypersonic flight.
Paramadhayalan P. +8 more
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Numerical Study of Transverse Injection into Supersonic flow of the Scramjet Combustor [PDF]
فناوری در مهندسی هوافضا, 2018 Nowadays efforts for development of the scramjet engines are increased. Scramjet engines use atmospheric oxygen as an oxidizer therefore they don’t need oxidizer tanks, thus the weight of these systems is less than comparable rocket systems.
Mostafa Zahedzadeh, Fathollah Ommi
doaj
Numerical Simulation of a Vortex Combustor Based on Aluminum and Steam
Energies, 2016 In this paper we report a new development in the numerical model for aluminum-steam combustion. This model is based on the diffusion flame of the continuum regime and the thermal equilibrium between the particle and the flow field, which can be used to ...
Xianhe Chen +3 more
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Ramjet Compression System for a Hypersonic Air Transportation Vehicle Combined Cycle Engine
Energies, 2018 This report assesses the performance characteristics of a ramjet compression system in the application of a hypersonic vehicle. The vehicle is required to be self-powered and perform a complete flight profile using a combination of turbojet, ramjet and ...
Sasha Veeran +2 more
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Influence of helix angle on heat transfer characteristics of regenerative cooling in spiral channel
Case Studies in Thermal EngineeringA rapid solution method for spiral line and a one-dimensional (1-D) heat transfer calculation model for spiral regenerative cooling channels (RCCs) are proposed to clarify the influence of the helix angle on the heat transfer characteristics of spiral ...
Xinlin Liu +4 more
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Application of multi-extruded fuel injectors for mixing enhancement of hydrogen gas at scramjet engine: computational study. [PDF]
Sci Rep, 2023 Abdollahi SA +4 more
europepmc +1 more source
Applied SciencesRegeneratively cooled scramjets are successfully used as propulsion devices in hypersonic vehicles. During operation, scramjets experience acceleration. This special process causes a dynamic flow process, and heat transfer in the cooling channel commonly
Qing Xu +3 more
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