Lecture 6 - Fluid Mechanics Forces Flashcards
What do fluid mechanics forces result from? (give equation)
The action of pressure and shear stresses on the object.
F_–> = int_Swet [tau_–>dS] - int_Swet[p*n_–>dS]
S_wet - ?
tau_–> - ?
p - ?
n_–> - ?
S_wet - wetted surface area
tau_–> - viscous stress vector on the object
p - static pressure
n_–> - outward pointing surface normal vector
Why are the Navier-Stokes equations nonlinear?
Convective acceleration in the equations
Pressure forces are created… - ?
at the surface of a body due to collisions between molecules of the fluid and the surface of the body.
Shearing forces - ?
produced by fluid viscosity,
provide information how well momentum is transferred between adjacent layers of the fluid.
Lift coefficient
C_L = L/q_inf * S * l
Drag coefficient
C_D = D/q_infSl
Moment coefficient
C_M = M/q_infSl
q_inf - ?
1/2 * rho_inf * V_inf^2
S - ?
l - ?
S- reference area
l - reference length
what do capital letters for forces represent?
3D Geometries
what is an aerofoil?
wings with infinite span
Sources of drag for bird wings or fins and fish tails etc?
Skin Friction
Pressure drag
What causes skin friction?
shear stresses in the boundary layer
What causes pressure drag?
Wake - a front back asymmetric flow pattern caused by the
flow separation. Occurs on blunt bodies or aerofoils when the
angle of attack is too large.
Downwash - vortex induced velocity. It affects the effective
angle of attack.
What is a streamlined body?
Drag is dominated by a frictional component.
What is a bluff body?
When pressure forces dominate drag.
What is von Karman vortex street?
Wake consisting of a procession of equal-strength vortices, equally
spaced but alternating in sign.
Occurring behind bluff bodies, including flat plates normal to the
flow direction.
In which the vortices move downstream at a speed less than the
freestream velocity (the reduction in speed is inversely
proportional to the streamwise distance separating alternate
vortices).
Giving rise to an alternating lift force (changes sign + or −) on
the cylinder at the same frequency as that of the vortex
shedding
What is strouhal number?
St = eta * D/ V_inf