Ignition delay time in swirling supersonic flow
AM Tahsini - Acta Astronautica, 2013 - Elsevier
Supersonic hydrogen–air cylindrical mixing layer is numerically analyzed to investigate the
effect of inlet swirl on ignition delay time in scramjets. Combustion is treated using detailed …
effect of inlet swirl on ignition delay time in scramjets. Combustion is treated using detailed …
Turbulence and additive effects on ignition delay in supersonic combustion
AM Tahsini - Proceedings of the Institution of Mechanical …, 2013 - journals.sagepub.com
Numerical study of two-dimensional supersonic hydrogen–air mixing layer is performed to
investigate the effects of turbulence and chemical additive on ignition distance. Chemical …
investigate the effects of turbulence and chemical additive on ignition distance. Chemical …
Reduced-order JP-10 Pyrolysis and Oxidation Model Based on Molecular Beam Mass Spectrometry Data: Ignition Delay Predictions
G Simms, HK Chelliah - AIAA SCITECH 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0636. vid A global, one-step, JP-10
(96.5% exo-tetradhydrodicyclopentadiene) decomposition reaction model is derived from …
(96.5% exo-tetradhydrodicyclopentadiene) decomposition reaction model is derived from …
Numerical study of supersonic turbulent free shear layer mixing and combustion
Y Belyayev, A Naimanova, A Kaltayev… - International Journal of …, 2018 - ijmph.kaznu.kz
Numerical study of two-dimensional supersonic hydrogen-air mixing and combustion in free
shear layer is performed. The system of Favre-Averaged Naveir-Stokes equations for …
shear layer is performed. The system of Favre-Averaged Naveir-Stokes equations for …
Numerical study of supersonic turbulent free shear layer
Y Belyayev, A Kaltayev - International Journal of Mathematics and …, 2014 - ijmph.kaznu.kz
Numerical study of two-dimensional supersonic turbulent free shear layer is performed. The
system of Fa-vre-Averaged Naveir-Stokes equations for multispecies flow is solved using …
system of Fa-vre-Averaged Naveir-Stokes equations for multispecies flow is solved using …
Numerical study of combustion efficiency in supersonic free shear layer. Численное изучение полноты сгорания в сверхзвуковом свободном сдвиговом слое.
Y Belyayev - Journal of Mathematics, Mechanics and Computer …, 2013 - bm.kaznu.kz
Numerical study of two-dimensional supersonic hydrogen-air mixing and combustion in free
shear layer is performed. The system of Navier-Stokes equations for multispecies reacting …
shear layer is performed. The system of Navier-Stokes equations for multispecies reacting …
[引用][C] Ignition Time Delay in Swirling Supersonic Flow Combustion
AM Tahsini - International Journal of Aerospace and Mechanical …, 2012
[引用][C] Ignition Analysis in Supersonic Turbulent Mixing Layer
AM Tahsini - International Journal of Aerospace and Mechanical …, 2011
[引用][C] Nitrogen Effects on Ignition Delay Time in Supersonic Premixed and Diffusion Flames
AM Tahsini - International Journal of Mechanical and Mechatronics …, 2013
[引用][C] Ignition Studies of Hydrocarbon Fuels at High Mach Number Scramjet Conditions
L Arundell - 2018 - espace.library.uq.edu.au
Scramjets are a developing technology for the propulsion of hypersonic vehicles. There is
currently insufficient knowledge detailing internal flow, mixing, ignition and combustion …
currently insufficient knowledge detailing internal flow, mixing, ignition and combustion …