An Experimental Study of Kerosene Combustion in a Supersonic Model Combustor Using Effervescent Atomization [PDF]
, 2005 Investigation of kerosene combustion in a Mach 2.5 flow was carried out using a model supersonic combustor with cross-section area of 51 mm × 70 mm and different integrated fuel injector/flameholder cavity modules.
赵建荣 +6 more
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Some Effects of Hydrogen Self-Ignition and Combustion in Supersonic Flow
Eurasian Chemico-Technological Journal, 2014 Results are presented of computational and experimental investigations of the influence of temperature and flow composition on the hydrogen combustion kinetics for a coaxial fuel supersonic flow.
U. Zhapbasbayev +4 more
doaj +1 more source
External hot surface axisymmetric models for supersonic combustion [PDF]
, 2016 An external axisymmetric configuration is introduced for supersonic combustion research in hypersonic wind tunnel flow. In this configuration, high quality data can be generated for validation of computational simulations.
Zhao, Mengmeng
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Effect of ramp-cavity on hydrogen fueled scramjet combustor
Propulsion and Power Research, 2014 Sustained combustion and optimization of combustor are the two challenges being faced by combustion scientists working in the area of supersonic combustion.
J.V.S. Moorthy +3 more
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Aerospace, 2023 In the combustion chamber of scramjets, fuel jets interact with supersonic airflow in the form of a liquid jet in crossflow (LJIC). It is difficult to achieve adequate jet–crossflow mixing and the efficient combustion of fuel in an instant.
Donglong Zhou +2 more
doaj +1 more source
An Analytical and Computational Investigation of Shock-Induced Vortical Flows with Applications to Supersonic Combustion [PDF]
, 1991 The motivation for study of shock-induced vortical flows is the problem of achieving rapid and efficient mixing of fuel and oxidizer in a SCRAMJET engine.
Yang, Joseph
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Longitudinal DC Discharge in a Supersonic Flow: Numerical Simulation and Experiment
Energies, 2022 This work focuses on detailed descriptions of DC discharge properties in supersonic airflow and its applicability in combustion simulations. Due to the complexity of obtaining most of the data in the experiment, our experimental research was supplemented
Alexander Firsov +5 more
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Large Eddy simulation of supersonic combustion using the eulerian stochastic fields method [PDF]
, 2019 The development of supersonic combustion engines (scramjet-type) presents several challenges. Numerical simulations of scramjet engine combustion have become an attractive alternative to experimental investigations.
Almeida, YP, Navarro-Martinez, S
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Experimental Investigation on Flameholding Mechanism and Combustion Performance in Hydrogen-Fueled Supersonic Combustors [PDF]
, 2002 Supersonic H-2/air combustion experiments of a fixed entry Mach number 2.5 were conducted using eight different model combustors, at various stagnation conditions and global equivalence ratios.
Han B +6 more
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Supersonic mixing and combustion: advance in les modeling [PDF]
Progress in Propulsion Physics, 2009 Mixing and combustion in supersonic reacting flows are currently under investigation for new generation launchers and trans-atmospheric vehicles. Experimental results with hydrogen injected at Mach 2.5 in a Mach 2 airstreams showed combustion taking place just in ∼0.6 m: this indicates that supersonic combustion is feasible within short combustors ...
INGENITO, ANTONELLA, BRUNO, Claudio
openaire +2 more sources