Boundary Layer Flow 16 - Turbulent Boundary Layer Flashcards

1
Q

Differences in laminar and turbulent mean velocity profiles

A

Through a pipe - laminar is parabolic curve, turbulent is shallower curve at end of profile
Over a plate - laminar is steeper, turbulent is lower and more curved

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2
Q

Why use mean quantities?

A

Instantaneous fluctuations vary ‘randomly’ in space and time

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3
Q

Reynolds decomposition

A

Mean + fluctuations

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4
Q

Streamwise mean momentum balance

A

Substitute Reynolds decomposition into NS and take mean

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5
Q

Total shear stress

A

Viscous stress + Reynolds stress

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6
Q

Turbulent BL velocity profile

A

Viscous wall layer - viscous shear dominates
Overlap layer - viscous and turbulent shear forces equally important
Outer layer - fully turbulent region, turbulent shear dominates, no direct effect of viscosity on mean flow

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7
Q

Important parameters close to wall

A

Viscosity
Wall shear stress
Density

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8
Q

Local Reynolds number

A

Measure of the relative importance of viscous and turbulent processes

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9
Q

Viscous wall layer

A

Local Reynolds number < 50
Velocity must be dependent on vertical distance, wall shear stress, density and viscosity

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10
Q

Viscous sublayer

A

Local Reynolds number < 5
Very close to wall and very thin
Assume velocity changes nearly linearly with distance from the wall, so velocity gradient is constant

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11
Q

Outer (velocity defect) layer

A

Local Reynolds number > 50
Velocity defect is independent of kinematic viscosity but depends on distance from wall relative to thickness, shear stress at interface with viscous sublayer and fluid density

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12
Q

Define velocity defect

A

Local reduction in velocity from free stream value

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13
Q

Overlap layer

A

30 < local Reynolds number < 0.1 x outer region Reynolds number

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14
Q

Log law

A

Approximates nearly entire velocity profile

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15
Q

Law of the wall

A

Used for viscous sublayer

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16
Q

Buffer layer

A

Region between viscous sublayer and log law region

17
Q

Power law

A

Used in addition to Log law to approximate turbulent BL velocity profile
1/7 power law is most popular, but close to wall is inaccurate for wall stress calculation

18
Q

Laminar/turbulent BL thickness on flat plate

A

1/7 power law for turbulent and Blasius for laminar
Shows turbulent BL is thicker than laminar BL

19
Q

Friction on a flat plate

A

Wall friction significantly higher for turbulent than laminar BL
BL transition increases friction significantly