Eliminating Boundary Layer Separation on a Cylinder with Nonuniform Suction [PDF]
International Journal of Aerospace Engineering, 2020 Boundary layer separation negatively influences the performance of aerospace vehicles, for example, by triggering static stall or reducing combustion engine efficiency.
James Ramsay +2 more
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Boundary layer separation and reattachment detection on airfoils by thermal flow sensors. [PDF]
Sensors (Basel), 2012 Sturm H +4 more
europepmc +2 more sources
An ODE for boundary layer separation on a sphere and a hyperbolic space [PDF]
Physica D: Nonlinear Phenomena, 2014 Chi Hin Chan +2 more
exaly +2 more sources
Is a baseball like knuckleball possible in cricket?
Flow, 2023 The knuckleball is considered to be one of the hardest pitches to hit in baseball due to its seemingly unpredictable motion. It has gained popularity in cricket in recent times.
Kunjal Shah, Sanjay Mittal
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Comparison of the Models for Multiscale Elastohydrodynamic Lubrication in a Line Contact [PDF]
Journal of Applied Fluid Mechanics, 2022 Two models are compared for calculating the surface separation in a multiscale elastohydrodynamic lubricated line contact for the same operating conditions.
W. Lin, J. Li, Y. Zhang
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Unsteady Motion of Shock Wave for a Supersonic Compression Ramp Flow Based on Large Eddy Simulation
Frontiers in Energy Research, 2022 A large eddy simulation (LES) is conducted to investigate shock wave/turbulent boundary layer interaction in a 24° compression ramp at a high inlet Mach number of Ma=2.9.
Xing Huang +3 more
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Numerical Investigation of Mach 2.5 Axisymmetric Turbulent Shock Wave Boundary Layer Interactions
Aerospace, 2023 Shock wave boundary layer interactions are common to both supersonic and hypersonic inlet flows. Wall-resolved implicit large-eddy simulations of a canonical Mach 2.5 axisymmetric shock wave boundary layer interaction experiment at Glenn Research Center ...
John-Paul Mosele +2 more
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Turbulent Boundary Layer Separation Control Using Magnetohydrodynamic Plasma Actuator
Aerospace, 2023 The pulse electric arc discharge in an external magnetic field is studied as a vortex generator in the subsonic boundary layer. A pulsed Ampere force induces a hairpin vortex near the wall; its structure depends on the relative direction of arc ...
Alexander Kotvitskii +2 more
doaj +1 more source
On injection-ejection fluid influence through different accelerating porous surfaces on unsteady 2d incompressible boundary layer characteristics [PDF]
Theoretical and Applied Mechanics, 2005 Through the porous contour in perpendicular direction, the fluid of the same properties as incompressible fluid in basic flow, has been injected or ejected with velocity who is a function of the contour longitudinal coordinate and time. The corresponding
Ivanović Dečan, Ivanović Vladan
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Aerospace, 2023 A shock wave/boundary layer interaction (SWBLI) is a common phenomenon in supersonic inlet flow, which can significantly degrade the aerodynamic performance of the inlet by inducing boundary layer separation.
Mengge Wang +6 more
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