you guys have officially confused the heck out of me
Can't we use the bernoulli equation to do this, for flowing pipes?
So...pressure = density(rho) * g * h
Bernoilli Eqn for a flowing fluid:
Some Constant = P * (rho*g*h) * (1/2 * rho * V^2)
P = the potential difference across the sytem, as in the circulatory system
(rho*g*h) = The elevation head of flow...or as we know it, pressure itself that we're talking about. This decreases as the next term(velocity) increases.
(1/2 * rho * v^2) = The velocity head of flow...or as we know it, the velocity itself. This increases as the above term(pressure) decreases, because it's gotta maintain that constant on the other side of the equation.
So we're saying here that the elevation head(pressure) and the velocity head are inversely proportional.
Now for the circulatory system, there is a base pressure difference(kinda like a voltage difference) across the entire system. It's as manfood said...I believe as well that the pressure in the capillaries is simply somewhere in between that in the aorta, and that in the venules, because it's a continuum. That takes care of pressure, don't relate it to the next paragraph.
Now we look at the continuity equation, A1v1 = A2v2 and see that since the capillaries have the largest cross sectional area, the blood velocity in them is lowest.
I probably got all that wrong and fed you guys a bunch of BS but please correct me ;O
Shriiiikeeeeeeee *does summoning dance thing*
edit: You can also use the bernoilli equation to show why a plane can fly, because air has to flow in equal amounts of time across the wing to maintain the flow rate. Since the path above the wing is greater than the path below the wing
_______________
/______________ \ <---airplane wing
The velocity has to be faster above the wing(meaning lower pressure), and since there's lower pressure above the wing, we get lift