Amanote Research
Register
Sign In
Discover open access scientific publications
Search, annotate, share and cite publications
Publications by A. V. Panina
On the Oblique Breakdown Mechanism in a Supersonic Boundary Layer on a Swept Wing at Mach 2
To the Analysis of the Natural Pulsation Development During Laminar-Turbulent Transition in Supersonic Boundary Layer
Related publications
Direct Numerical Simulation of a Supersonic Turbulent Boundary Layer at Mach 2.5
Journal of Fluid Mechanics
Mechanics of Materials
Condensed Matter Physics
Mechanical Engineering
Transient Growth in Oblique Shock Wave/Laminar Boundary Layer Interactions at Mach 5.92
Two-Dimensional Surface Irregularities on Swept Wing Boundary-Layer Transition: Forward Facing Steps
Large-Eddy Simulation of Laminar-Turbulent Transition in a Swept-Wing Boundary Layer
Laminar—Turbulent Transition in a Supersonic Boundary Layer
Physics of Fluids
Mechanics of Materials
Condensed Matter Physics
Mechanical Engineering
Fluid Flow
Transfer Processes
Computational Mechanics
Numerical Simulation on the Development of Periodic Three-Dimensional Disturbances in a Supersonic Boundary Layer
EPJ Web of Conferences
Astronomy
Physics
Plate-Injection Into a Separated Supersonic Boundary Layer
Journal of Fluid Mechanics
Mechanics of Materials
Condensed Matter Physics
Mechanical Engineering
The Effect of Mach Number on Unstable Disturbances in Shock/Boundary-Layer Interactions
Physics of Fluids
Mechanics of Materials
Condensed Matter Physics
Mechanical Engineering
Fluid Flow
Transfer Processes
Computational Mechanics
Coupling Between a Supersonic Boundary Layer and a Flexible Surface
AIAA Journal
Aerospace Engineering
