Fluid Dynamics Flashcards

1
Q

Fluid

A
  • Flows under the action of forces, while deforming ‘continuously’ for as long as force is applied.(lacks ability to offer resistance to a deforming force)
  • force acting on solid produces a change in shape (small strain) only remains as long as force is applied
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2
Q

Shear stress

A

t=u*(du/du)

t=sheer stress
u=viscosity
du=rate of strain (speed)
du=perpendicular distance from fixed surface

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3
Q

Viscosity

A

Measure of a liquids resistance to flow

High viscosity>thick fluid (like honey)>low flow rate

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4
Q

Viscosity in gases and liquids

A
  • in gas if temp increase the collision frequency increases hence increasing viscosity
  • in liquid when temp increases the separation between molecules increases hence viscosity decreases. (High pressure also affects it unlike gases)
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5
Q

Kinematic viscosity

A

•kinematic viscosity defined as ratio u/p (absolute viscosity/fluid density)

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6
Q

surface tension

A

The property of a liquid that lets insects walk on water defined as the force per unit length surface tension (N/m unit)

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7
Q

Capillarity

A

If a open tube at both ends is lowered vertically into a liquid the level of liquid will rise along the tube

Concave meniscus water

Co’vex does like it self so opposite direction

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8
Q

Pressure

A

Hydraulic lift- pressure kept constant and area changed so less force needed to push car up.

When pushing down 1/1=p constant=10000/10000

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9
Q

Vapour pressure

A

•vapour pressure (space is confined equilibrium will be reached then molecules produce this vapour pressure)

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10
Q

Cavitation

A

cavitation low pressure to higher pressure forms bubbles to access this regions

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11
Q

Bulk modulus

A

For liquids K tends to suffer a small change because they are incompressible meaning no change of volume unlike gases

K=-V(dP/dV) = p(dP/dp)

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12
Q

Bernoulli’s equation

A

Sum of the pressure, kinetic and potential energy is always constant for an ideal incompressible and non viscous fluid having stream line steady flow (stream line not changing with time)

No heat loss or added to system
No energy lost to friction
No energy lost in fluid

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13
Q

Continuity equation

A

Mass flow conserved-

p1 A1 v1 =p2 A2 v2

Volume continuity if fluid is incompressible:

A1 v1 = A2 v2

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14
Q

Verna contracta

A

If the exit around the hole is not curved and is sharp then the diameter of the jet (stream line exiting) will be less than of the hole. Which means not constant pressure thus no uniform velocity

Cc(contraction coefficient)=area of stream/area of hole

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15
Q

Stream line

A

The tangent of the velocity vectors of each particles path in a steady flow

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