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Combined influence of coating permeability and roughness on supersonic boundary layer stability and transition

Journal of fluid mechanics, 2016-07, Vol.798, p.751-773

2016

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Experimental Investigation of the Structure of Disturbances from Two Pulsed Sources in the Flat-Plate Supersonic Boundary Layer

Fluid dynamics, 2023-08, Vol.58 (4), p.532-541

2023

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Achievements and problems of research on the development of controlled disturbances from a glow discharge in supersonic boundary layers

AIP Conference Proceedings, 2020, Vol.2288 (1)

2020

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Experimental and numerical investigation of controlled disturbances development from two sources in supersonic boundary layer

Advances in aerodynamics, 2019-07, Vol.1 (1), p.14-13, Article 14

2019

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Experimental study of impact of a weak shock waves on a supersonic flow in the boundary layer of the swept plate

AIP Conference Proceedings, 2023, Vol.2504 (1)

2023

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Features of the cross-correlation characteristics of disturbances in the supersonic boundary layer of the plate at the influence of a pair of weak shock waves on the leading edge

Thermophysics and aeromechanics, 2024-01, Vol.31 (1), p.15-28

2024

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Effect of the slot depth on supersonic boundary-layer stabilization

Thermophysics and aeromechanics, 2024-01, Vol.31 (1), p.71-78

2024

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Experimental study of the relationship between the pulsations of the oncoming flow and the disturbances of the boundary layer of a sharp plate at Mach number M=2.5

AIP Conference Proceedings, 2023, Vol.2504 (1)

2023

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On a laminar-turbulent transition on swept wings with subsonic and supersonic leading adge

AIP Conference Proceedings, 2023, Vol.2504 (1)

2023

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Experimental study of influence of heavy gas injection into boundary layer on perforated model surface at Mach number 2 on its stability to controlled disturbances

AIP Conference Proceedings, 2021, Vol.2351 (1)

2021

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Experimental studies of pulsations of the boundary layer of swept wings with periodic roughness at M = 4

AIP Conference Proceedings, 2023, Vol.2504 (1)

2023

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Cross-correlation measurement of disturbance initiated by weak shock wave in the flat plate boundary layer with blunt leading edge at Mach 2

AIP Conference Proceedings, 2021, Vol.2351 (1)

2021

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EXPERIMENTAL STUDY OF EVOLUTION OF CONTROLLED PERTURBATIONS IN A LONGITUDINAL VORTEX GENERATED IN A BOUNDARY LAYER ON A FLAT PLATE AT A MACH NUMBER M = 2

Journal of applied mechanics and technical physics, 2023-08, Vol.64 (4), p.656-666

2023

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The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate

Journal of physics. Conference series, 2019-11, Vol.1404 (1), p.12083

2019

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An effect of unit Reynolds number on the laminar-turbulent transition on 3D swept wing with χ = 72° at M = 2

AIP Conference Proceedings, 2021, Vol.2351 (1)

2021

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Experimental study of the laminar-turbulent transition in the boundary layer of the wing with a sweep angle of the leading edge of 72 degrees at Mach 4

AIP Conference Proceedings, 2021, Vol.2351 (1)

2021

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Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer at Mach 2-4

AIP Conference Proceedings, 2021, Vol.2351 (1)

2021

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Experimental investigation of natural disturbances of a supersonic boundary layer on a swept-wing model with periodic roughness at Mach 2.5

AIP Conference Proceedings, 2021, Vol.2351 (1)

2021

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"N-wave" propagation in supersonic flow at flow past the flat plate with sharp edge

Journal of physics. Conference series, 2019-11, Vol.1404 (1), p.12102

2019

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Influence of hydrogen on the localization of plastic strain in low-carbon steel

Steel in translation, 2016-12, Vol.46 (12), p.851-854

2016

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Influence of the leading-edge bluntness radius of a plate on the response of flat-plate boundary layer to an N-wave at Mach number M = 2

Thermophysics and aeromechanics, 2023-03, Vol.30 (2), p.227-237

2023

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Linear and nonlinear development of controlled disturbances in the supersonic boundary layer on a swept wing at Mach 2.5

Journal of physics. Conference series, 2016-10, Vol.754 (2), p.22005

2016

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Evolution of artificial disturbances in swept wing supersonic boundary layer

Journal of physics. Conference series, 2019-11, Vol.1404 (1), p.12084

2019

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The controlled periodic impact on the longitudinal vortex in the boundary layer at Mach 2

Journal of physics. Conference series, 2019-11, Vol.1404 (1), p.12094

2019

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Experimental investigation of freestream disturbances across an oblique shock wave via modal analysis with a wedge hot-film

Thermophysics and aeromechanics, 2019-11, Vol.26 (6), p.789-802

2019

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Combined influence of coating permeability and roughness on supersonic boundary layer stability and transition

Experimental Investigation of the Structure of Disturbances from Two Pulsed Sources in the Flat-Plate Supersonic Boundary Layer

Achievements and problems of research on the development of controlled disturbances from a glow discharge in supersonic boundary layers

Experimental and numerical investigation of controlled disturbances development from two sources in supersonic boundary layer

Experimental study of impact of a weak shock waves on a supersonic flow in the boundary layer of the swept plate

Features of the cross-correlation characteristics of disturbances in the supersonic boundary layer of the plate at the influence of a pair of weak shock waves on the leading edge

Effect of the slot depth on supersonic boundary-layer stabilization

Experimental study of the relationship between the pulsations of the oncoming flow and the disturbances of the boundary layer of a sharp plate at Mach number M=2.5

On a laminar-turbulent transition on swept wings with subsonic and supersonic leading adge

Experimental study of influence of heavy gas injection into boundary layer on perforated model surface at Mach number 2 on its stability to controlled disturbances

Experimental studies of pulsations of the boundary layer of swept wings with periodic roughness at M = 4

Cross-correlation measurement of disturbance initiated by weak shock wave in the flat plate boundary layer with blunt leading edge at Mach 2

EXPERIMENTAL STUDY OF EVOLUTION OF CONTROLLED PERTURBATIONS IN A LONGITUDINAL VORTEX GENERATED IN A BOUNDARY LAYER ON A FLAT PLATE AT A MACH NUMBER M = 2

The experimental study of the weak shock wave action on the boundary layer of the sweep flat plate

An effect of unit Reynolds number on the laminar-turbulent transition on 3D swept wing with χ = 72° at M = 2

Experimental study of the laminar-turbulent transition in the boundary layer of the wing with a sweep angle of the leading edge of 72 degrees at Mach 4

Investigation of laminar-turbulent transition of supersonic boundary layer by scanning constant temperature hot-wire anemometer at Mach 2-4

Experimental investigation of natural disturbances of a supersonic boundary layer on a swept-wing model with periodic roughness at Mach 2.5

"N-wave" propagation in supersonic flow at flow past the flat plate with sharp edge

Influence of hydrogen on the localization of plastic strain in low-carbon steel

Influence of the leading-edge bluntness radius of a plate on the response of flat-plate boundary layer to an N-wave at Mach number M = 2

Linear and nonlinear development of controlled disturbances in the supersonic boundary layer on a swept wing at Mach 2.5

Evolution of artificial disturbances in swept wing supersonic boundary layer

The controlled periodic impact on the longitudinal vortex in the boundary layer at Mach 2

Experimental investigation of freestream disturbances across an oblique shock wave via modal analysis with a wedge hot-film

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