Fluid Dynamics Flashcards
Fluid
- 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
Shear stress
t=u*(du/du)
t=sheer stress
u=viscosity
du=rate of strain (speed)
du=perpendicular distance from fixed surface
Viscosity
Measure of a liquids resistance to flow
High viscosity>thick fluid (like honey)>low flow rate
Viscosity in gases and liquids
- 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)
Kinematic viscosity
•kinematic viscosity defined as ratio u/p (absolute viscosity/fluid density)
surface tension
The property of a liquid that lets insects walk on water defined as the force per unit length surface tension (N/m unit)
Capillarity
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
Pressure
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
Vapour pressure
•vapour pressure (space is confined equilibrium will be reached then molecules produce this vapour pressure)
Cavitation
cavitation low pressure to higher pressure forms bubbles to access this regions
Bulk modulus
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)
Bernoulli’s equation
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
Continuity equation
Mass flow conserved-
p1 A1 v1 =p2 A2 v2
Volume continuity if fluid is incompressible:
A1 v1 = A2 v2
Verna contracta
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
Stream line
The tangent of the velocity vectors of each particles path in a steady flow