Results 31 to 40 of about 4,462 (234)
Energies, 2021 To investigate the combustion modes and unsteady characteristics during the condition transition of a scramjet combustor, a series of experiments were carried out under the condition of Mach 2.52 supersonic incoming flow, the corresponding stagnation ...
Dongpeng Jia +4 more
doaj +1 more source
Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity
Energies, 2019 Scramjet based on solid propellant is a good supplement for the power device of future hypersonic vehicles. A new scramjet combustor configuration using solid fuel, namely, the solid fuel rocket scramjet (SFRSCRJ) combustor is proposed.
Chaolong Li +4 more
doaj +1 more source
Simulation of Elliptical Liquid Jet Primary Breakup In Supersonic Crossflow
International Journal of Aerospace Engineering, 2020 The study of elliptical liquid jets in supersonic flow in a Mach 2.0 is performed numerically. The primary breakup process of the elliptical liquid jet is simulated for a Weber number 223, liquid/gas flux momentum 4.0.
Yao-zhi Zhou +3 more
doaj +1 more source
Effects of Oxygen Enrichment on Supersonic Combustion in a Mach 10 Scramjet [PDF]
, 2021 Scramjet engines are a suitable replacement for rockets in access-to-space systems, but, being air-breathing engines, their operational envelope is limited to altitudes where enough oxygen is available for combustion.
Wheatley, Vincent +3 more
core +1 more source
Aerospace, 2023 Supersonic combustion instability studies are crucial for the future maturation of scramjet engines. In the present paper, the supersonic combustion instability in a strut-based scramjet combustor is investigated through large eddy simulation and dynamic
Yuwei Cheng +3 more
doaj +1 more source
The Combustion Characteristics of Double Ramps in a Strut-Based Scramjet Combustor
Energies, 2021 This paper focuses on the influence of ramp locations upstream of a strut-based scramjet combustor under reacting flow conditions that are numerically investigated. In contrast, a computational study is adopted using Reynolds Averaged Navier Stokes (RANS)
A. Antony Athithan +4 more
doaj +1 more source
A Mixing Process Influenced by Wall Jet-Induced Shock Waves in Supersonic Flow
Applied Sciences, 2022 With the development of hypersonic air-breathing propulsion systems, such as the supersonic combustion ramjet (Scramjet) and rocket-based combined cycle (RBCC) engines, the mixing process of supersonic airstream with fuel in the engine combustor has been
Ji Zhang +3 more
doaj +1 more source
Effects of Sidewall Compression and Relaminarization in a Scramjet Inlet
, 2013 This paper presents the numerical simulations and the performance analysis of a scramjet inlet as part of a combined experimental and numerical study.
Hohn, Oliver +4 more
core +1 more source
, 2011 This paper presents the numerical simulations and performance analysis of a 3D scramjet inlet with focus on the effects of sidewall compression and relaminarization. A well-validated finite volume flow solver was used to simulate a scramjet inlet with a
Marek Behr +9 more
core +1 more source
Numerical study of detonation wave propagation modes in annular channels
AIP Advances, 2021 Modes of detonation wave propagation in annular channels were investigated numerically by using the adaptive mesh refinement technique. Two-dimensional, reactive Euler equations with a detailed hydrogen/oxygen reaction model were adopted in the ...
Duo Zhang +6 more
doaj +1 more source