an adverse pressure gradient ... not enoughto causesignificant boundary - layer separation
an adverse pressure gradient but not enoughto causesignificant boundary - layer separation
some roughness in certain locationsto causeboundary flow separation
adverse pressure gradientscauseboundary layer separation from their surfaces
by the drop - off(passive) caused byThe intentional boundary layer separation
an impulsively stretching plate and a coupled four - equation system that models the problem of unsteady MHD flow and mass transfer in a porous space(passive) caused byboundary layer flow
by stretching(passive) caused byboundary separation
conditions of separation in transonic flow ... shock wave and boundary layercan causeboundary layer separation
a strong effect on the flow dynamics ... are observedto causeboundary layer separation
the pressure rise at the shock ... sufficientto causeseparation of the laminar boundary layer
7 Boundary layer separation from a cylinder : flow left to rightcausesThe separation of the boundary layer
a strong shock present at the upper surface of the conventional airfoilto causea boundary layer separation
by the strong adverse pressure gradient of the shock(passive) caused byboundary layer separation
the appearance of a strong shock on the upper surface of the airfoilcausesboundary layer separation
a finite - core vortexleadingto unsteady separation in a boundary layer
presence of adverse pressure gradient(passive) is caused bySeparation of boundary layer
Viscous effects within the boundary layercauseboundary layer separation
by the adverse pressure gradients(passive) caused byboundary layer separation
in an improvement of the free volume of the separation layerresultedin an improvement of the free volume of the separation layer
in ridiculously erroneous snowfall mapsresultingin ridiculously erroneous snowfall maps
in a layer - separated structureresultsin a layer - separated structure
of a plasma polymer layercomposedof a plasma polymer layer
to lift - off failures if it is too large or too lowleadsto lift - off failures if it is too large or too low
to transition andleadsto transition and
in aerodynamic instabilities affecting repeatability and consistency of wind speed measurementresultingin aerodynamic instabilities affecting repeatability and consistency of wind speed measurement
to failure of the articlecould leadto failure of the article
from cell collapse and disintegrationresultsfrom cell collapse and disintegration
in artifacts in the display image , such as undesirable bright lines in the display imagewould resultin artifacts in the display image , such as undesirable bright lines in the display image
large energy losses and strong adverse pressure gradientscauseslarge energy losses and strong adverse pressure gradients
from a tendency of the product to stick to the other die as the dies are separated from one anotherresultsfrom a tendency of the product to stick to the other die as the dies are separated from one another
to a reduction in turbulence and frictional dragleadingto a reduction in turbulence and frictional drag
the side forcecausesthe side force
in increased dragresultsin increased drag
all the limitations(passive) set byall the limitations
in a smaller wakeresultsin a smaller wake
meltingto causemelting
Sika levelling and/or(passive) are designedSika levelling and/or
air - flow over aircraft surfacesInfluencingair - flow over aircraft surfaces
in decrease of pressure dragresultingin decrease of pressure drag
from a source of momentum and buoyancy Boundary layeroriginatingfrom a source of momentum and buoyancy Boundary layer
an INCREASE in dragcausesan INCREASE in drag
stall resulting in a low efficiencycan causestall resulting in a low efficiency
a large pressure difference forming the wake flow of the cylindercausesa large pressure difference forming the wake flow of the cylinder
in a reduction in dragresultsin a reduction in drag
the associated rise in aerodynamic drag(passive) caused bythe associated rise in aerodynamic drag