Air Flow Visualization Flashcards

(46 cards)

1
Q

Movement of liquids and gases in response to forces

A

fluid flow

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2
Q

The property of a fluid that describes its resistance to shear deformation or internal friction.

A

viscosity (μ)

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3
Q

Measures how strongly fluid layers resist sliding past each other

A

viscosity (μ)

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4
Q

Measures internal resistance of fluid to shear

A

dynamic viscosity (μ)

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5
Q

Measures the resistive flow of a fluid when no external force is applied except the influence of weight

A

kinematic viscosity (ν)

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6
Q
  • Viscosity effects are ignored.
  • Used in high Reynolds number flows where inertial forces dominate.
  • Provides quick estimation of aerodynamic forces.
A

inviscid flow

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7
Q
  • Viscosity effects are important.
  • Internal friction and shear stresses affect the flow.
  • Important near solid surfaces.
A

viscous flow

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8
Q
  • Fluid particles move in smooth parallel layers.
  • Minimal mixing between layers.
  • Occurs at low Reynolds numbers.
A

laminar flow

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9
Q
  • Fluid motion is irregular and chaotic.
  • Strong mixing between layers.
  • Occurs at high Reynolds numbers.
A

turbulent flow

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10
Q

The thin region of fluid close to a surface where viscous effects are significant

A

boundary layer

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11
Q
  • Velocity changes from zero at the wall to the free-stream velocity.
  • Caused by the no-slip condition, where the fluid sticks to the surface.
A

boundary layer

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12
Q

A measure of the ratio of inertia forces to viscous forces

A

Reynolds number

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13
Q

Can be used to assess how comparable the aerodynamic flows are in a body and its scaled counterpart

A

Reynolds number

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14
Q

Can be used to determine whether the boundary layer is turbulent or laminar in whole or in part

A

Reynolds number

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15
Q

Shows how fluid velocity changes from the wall to the free stream

A

velocity profile

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16
Q

At the wall: velocity = _ (no-slip condition)

A

0

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17
Q

Away from the wall: velocity _ until it reaches free-stream velocity.

A

increases

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18
Q

Characteristics:
- Smooth and orderly velocity distribution.
- Velocity increases gradually from the wall.

A

Laminar Boundary Layer Velocity Profile

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19
Q

Characteristics:
- Velocity profile is fuller and steeper near the wall.
- Strong mixing of fluid layers.

A

Turbulent Boundary Layer Velocity Profile

20
Q

A point in the flow where it changes or “transitions” from laminar flow to turbulent flow

A

transition point

21
Q

Its location in the chord is indicated by the critical chord x_cr derived from the critical Reynolds number.

A

transition point

22
Q
  • Studies focus on shear forces, pressure forces, and heating loads that a fluid flow exerts on a solid surface.
  • Flow pattern visualization near or on the surface aids these studies.
  • Surface coating methods are commonly used, where a material interacts with the flow to provide visible data.
  • Interaction types: mechanical, chemical, or thermal.
A

surface flow patterns

23
Q

Standard technique for decades in wind tunnel studies

A

oil film visualization

24
Q

Method:
- Surface coated with thin oil layer containing finely powdered pigment.
- When airflow starts, oil moves with the air, leaving pigment streaks on the surface.

A

oil film visualization

25
Purpose: - Streak patterns indicate flow direction near the surface. - Specific features in the pattern reveal flow separation or flow reattachment points.
oil film visualization
26
Method: Short tufts attached to the surface of interest
wall tufts
27
Tufts align with local flow direction
Laminar, attached flow
28
Tufts show unsteady motion
Unsteady or turbulent flow
29
Method: Coating surface with sublimating materials (e.g., naphthalene or azobenzene)
mass transfer
29
Tufts exhibit violent motion or tend to lift off the surface
Separated flow
30
Mechanism: Material evaporates into the airflow, visualizing mass transfer between the surface and fluid
mass transfer
31
- Luminescent dye (luminophore) dispersed in oxygen-permeable binder. - Excitation: Illuminated with short-wavelength light (blue or UV). - Mechanism: Collisions between luminophores and oxygen reduce emitted light intensity. - Output: Light intensity variations reveal wall pressure distribution.
pressure sensitive paint (PSP)
32
- Similar principle as PSP but without oxygen quenching. - Measures wall temperature distribution instead of pressure.
temperature sensitive paint (TSP)
33
Injection of Foreign Materials for Flow Visualization
tracer particles
34
Method: Introduce a visible material into the flow. - Air flows: commonly use smoke - Water flows: commonly use dye
tracer particles
35
Purpose: - Track specific flow lines downstream of the injection point. - Fill a flow region to visualize boundaries and geometric extension of the flow regime. - Particularly useful for visualizing flow separation.
tracer particles
36
Common Techniques: - Smoke visualization - Dye visualization in water
tracer particles
37
Includes steam, vapor, mist, and aerosols, not just combustion products
smoke
38
Desired tracer properties: - Neutrally buoyant (follows the flow accurately) - Non-toxic (safe for use) - Low mixing with the main fluid (maintains clear visualization of flow paths)
smoke visualization
39
- neutral buoyancy - high stability against mixing - good visibility
visualization by dye in water
40
Principle: Fluid density affects its refractive index. Application: Variations in refractive index reveal density changes due to: - Compressibility - Thermal effects - Mixing of fluids with different densities
optical methods
41
Common uses: High-speed wind tunnels, ballistic ranges, shock tubes. Common Techniques: - Shadowgraph - Schlieren
optical methods
42
Simplest optical flow visualization technique (first explored by Dvorak)
Shadowgraph
43
Setup: Only requires a light source; no lenses or mirrors needed. Principle: Variations in refractive index produce visible shadow patterns. Applications: - Open-air visualization using sunlight. Examples: - Rising warm air - Benzene vapor projections - Shock wave visualization
Shadowgraph
44
Enhanced optical technique derived from Shadowgraph, more sensitive to density changes
Schlieren system
45
Principle: Detects first-derivative of density, making it more sensitive than Shadowgraph Setup: - Parallel light beam is converged by a lens or spherical/parabolic mirror (“Schlieren head”). - Knife edge at focal point blocks part of light, creating contrast based on density gradients. - Camera focuses the flow field onto a recording plane to eliminate unwanted shadows. Application: Visualization of fine density variations in gases (e.g., shock waves, thermal flows).
Schlieren system