Ch 3 - Describing And Understanding Airflow Flashcards

1
Q

Equation of Continuity

A

Works on the principle that mass cannot be created or destroyed -> A constant mass flow

-> Air mass flow entering a stream tube must remain the same at all points along it

AVp = Mass Flow = Constant Value

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2
Q

Bernoulli’s Theorem

A

Works on the principle that energy cannot be created or destroyed, only changed from one form to another.

The sum of the static pressure + the kinetic energy (per unit volume) = Constant

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3
Q

Total Pressure =

A

= Static Pressure + Dynamic Pressure

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4
Q

The 3 types of airflow:

A
  • Laminar (smooth, uniform)
  • Turbulent (unsteady)
  • Vortex (elements of laminar and turbulent)
    • > Steady flow on a helical path which eventually dissipates
    • > Detailed flow may be turbulent

Loses energy to surrounding air
-> Becomes slower and larger before this happens

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5
Q

Ideal Fluid Properties

A
  • > Incompressibility

- > No Viscosity

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6
Q

Venturi Effect

A

When airflow lines get converge together, increasing in speed and then diverge losing speed

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