Dynamics of a supersonic transitional flow over a backward-facing step
The transition mechanism and unsteady behavior behind a backward-facing step (BFS) in
the supersonic regime at Ma= 1.7 and Re δ 0= 13 718 is investigated using large-eddy …
the supersonic regime at Ma= 1.7 and Re δ 0= 13 718 is investigated using large-eddy …
Influence of upstream disturbances on the primary and secondary instabilities in a supersonic separated flow over a backward-facing step
The development of primary and secondary instabilities is investigated numerically for a
supersonic transitional flow over a backward-facing step at Ma= 1.7 and R e δ 0= 13 718 …
supersonic transitional flow over a backward-facing step at Ma= 1.7 and R e δ 0= 13 718 …
Effect of the wave structure of the flow in a supersonic combustor on ignition and flame stabilization
MA Goldfeld, YV Zakharova, AV Fedorov… - … , Explosion, and Shock …, 2018 - Springer
Results of numerical and experimental investigations of a high-velocity flow in a plane
channel with sudden expansion in the form of a backward-facing step, which is used for …
channel with sudden expansion in the form of a backward-facing step, which is used for …
Structures and aero-optical effects of supersonic flow over a backward facing step with vortex generators
Y Zhu, S Yi, H Ding, W Nie, Z Zhang - European Journal of Mechanics-B …, 2019 - Elsevier
Based on nano-tracer based planar laser scattering (NPLS) and background oriented
schlieren (BOS) based wavefront sensing (BOS-WS), the fine structures and aero-optical …
schlieren (BOS) based wavefront sensing (BOS-WS), the fine structures and aero-optical …
Experimental and numerical investigation on initial flame kernel blow-out in a supersonic combustor with a rear-wall-expansion cavity flameholder
T Wang, Y Yang, Z Wang, Z Cai, M Sun, G Li - Acta Astronautica, 2019 - Elsevier
The initial flame kernel blow-out process in an ethylene fueled scramjet combustor with a
rear-wall-expansion cavity was investigated experimentally and numerically. In the …
rear-wall-expansion cavity was investigated experimentally and numerically. In the …
Влияние волновой структуры течения в сверхзвуковой камере сгорания на воспламенение и стабилизацию горения
МА Гольдфельд, ЮВ Захарова, АВ Федоров… - Физика горения и …, 2018 - mathnet.ru
Представлены результаты численных и экспериментальных исследований
высокоскоростного течения в плоском канале с внезапным расширением в виде …
высокоскоростного течения в плоском канале с внезапным расширением в виде …
A numerical study to reduce the drag effects in hypersonic flow over the backward facing step
A Sivan, D Saravanan, YS Rammohan - Materials Today: Proceedings, 2022 - Elsevier
A numerical simulation study of laminar hypersonic cold airflow over the backward-facing
step (BFS) is performed at a freestream Knudsen number of 0.00009589 for resolving the …
step (BFS) is performed at a freestream Knudsen number of 0.00009589 for resolving the …
Numerical simulation of hydrogen mixing and combustion in a supersonic combustor chamber
NN Fedorova, MA Goldfeld… - AIP Conference …, 2018 - pubs.aip.org
The results of numerical and experimental investigations of hydrogen mixing and ignition
processes in a supersonic combustion chamber with backward facing steps located on the …
processes in a supersonic combustion chamber with backward facing steps located on the …
[图书][B] Numerical study of hot jet ignition of hydrocarbon-air mixtures in a constant-volume combustor
A Karimi - 2014 - search.proquest.com
Ignition of a combustible mixture by a transient jet of hot reactive gas is important for safety of
mines, pre-chamber ignition in IC engines, detonation initiation, and in novel constant …
mines, pre-chamber ignition in IC engines, detonation initiation, and in novel constant …
[PDF][PDF] Shock wave-boundary layer interaction in a transitional flow over a backward-facing step
The unsteadiness of shock wave-boundary layer interactions is investigated in a transitional
backward-facing step flow at Ma= 1.7 and Reδ0= 13718 using large eddy simulation. The …
backward-facing step flow at Ma= 1.7 and Reδ0= 13718 using large eddy simulation. The …