|
|
|
|
|
|
mass density (metric) |
|
|
|
|
|
weight density |
|
|
|
|
|
|
|
|
|
|
specific gravity - ratio of the density of the
substance to the density of water |
|
adhesion - attraction between unlike molecules |
|
cohesion - attraction between like molecules |
|
surface tension - due to cohesive forces in
fluid when the shape is changed |
|
capillary action - due to adhesive forces and
the surface tension |
|
Viscosity - the internal resistance of a fluid |
|
|
|
|
|
force per unit of area |
|
|
|
|
|
may be due to the weight (density) of a fluid
and the depth. |
|
|
|
|
|
|
|
|
Buoyancy - apparent weight difference of an
object submerged in a liquid due to the pressure difference from top to
bottom |
|
Archimedes’ principle - an object in a fluid is
buoyed up with a force equal to the weight of the volume of fluid displaced |
|
|
|
|
Pascal’s principle - pressure applied to an
enclosed fluid is transmitted undiminished to every portion of the fluid
and to the walls of the container |
|
|
|
|
|
|
|
|
Fluid Flow |
|
Assumptions: |
|
streamline |
|
incompressible |
|
nonviscous |
|
Flow rate (R) |
|
|
|
|
Constant flow rate – the flow rate in (1) must
equal the flow rate out (2) |
|
|
|
|
|
Bernoulli’s Equation |
|
|
|
|
|
P = absolute pressure |
|
r = mass density |
|
g = acceleration of gravity |
|
h = height (depth) |
|
v = velocity |
|
|
|
|
|
Applications of Bernoulli’s Equation |
|
Fluids at rest |
|
|
|
|
|
Flow from a small hole in a large tank |
|
|
|
|
|
Venturi meter |
|
|
|
|
Lift (force) on an airplane wing |
|
|
|
|
|
|
|
The air speed past the upper surface of a wing
is 352 km/h (98 m/s) and past the lower surface is 320 km/h (89 m/s). The
density of air is 1.21 kg/m3. Determine the lift on a wing with
area of 38 m2. |
|
F = ? |
|
v1 = 98 m/s v2 = 89 m/s r = 1.21 kg/m3
A=38 m2 |
|
DP = 1/2
r Dv2 F = DP A |
|
DP = 1/2
(1.21) (982 -892) =
1018 N/m2 |
|
F = 1018 (38) = 38700 N (approx. 8700 lbs) |
|