Hemodynamics Flashcards
State the relationship between total peripheral resistance and blood flow; given two values, calculate the unknown quantity.
NOTE, DO NOT MEMORIZE EQUATIONS, THEY ARE GIVEN ON TEST (do understand them)–DO MEMORIZE THIS: Please understand that
you will need to know other equations that involve cardiac output, MAP, pulse pressure, and TPR.
P (delta) = Q x R
delta = Paorta - Pr atrium or Pleft ventricle - Pright atrium
1/TPR = 1/R1 + 1/R2 …. + 1/Rn
R-organ = R1 + R2 + R…. + Rn
Describe laminar and turbulent flow characteristics, define the critical velocity and the transition from one type of flow to another.
Laminar flow, where flow Q is proportional to ΔP, breaks down when velocity reaches a critical point. Above this velocity, the flow depends less strongly on pressure gradient, rather:
Q~(ΔP)^1/2 in turbulent flow
This is because the effective resistance increases. This region is called turbulent flow which causes significant losses of kinetic energy. In turbulent flow, Q is proportional to the square root of ΔP. For the same ΔP, there is less flow when flow is turbulent than when laminar.
Describe the sounds of turbulent flow and their relationship to clinical measurements.
Clinically, the distinction between laminar and turbulent flow is very important since laminar flow is silent while turbulent flow generates sound.
Murmurs are audible sounds due to vibrations in heart or vessel walls.
Korotkoff sounds of sphygmomanometry (blood pressure measurement with inflatable cuff) are also examples of the sound of turbulent flow.
Describe the relationship between pressure and stress on the blood vessel wall.
As pressure increases (stenosis or volume decreases), stress increases = they are directly proportional
Sheer stress is created by flowing blood on the endothelial wall directed along the long axis of the vessel. The velocity profile in a rigid cylindrical tube is parabolic. The outermost layer has zero velocity & highest stress because friction is greatest at the wall (center of the tube has highest velocity & least stress).
Stenotic vessels (especially @ bifurcations = highest areas of athlerosclerosis) have turbulent flow with a lot of stress.
Poisielles Law
Q=ΔP/R=ΔP(πr^4/8ηL)
dP = deltaP = pressure drop
CO, cardiac output is approximately equal to what variable (MEMORIZE)?
Q, flow
Equation for total peripheral resistance, TPR (MEMORIZE)
1/TPR = 1/Rbrain + 1/Rkidney + … 1/Rn
The overall resistance to flow through the circulation is called the total peripheral resistance (TPR). The organs are arranged in parallel network, the resistance of each organ contributes to the TPR according to the inverse relationship. By this mechanism blood flow is regulated and balanced throughout the body according to organ needs.
TPR = mm Hg/ml/s
MAP (MEMORIZE, 2 equations) =
MAP = CO x TPR
MAP = DP + 1/3(SP-DP)
For the body, delta P is equal to
Pressure in left ventricle
Flow in series of tubes
is constant Q = Q1 = Q2 = Qn
Flow in parallel tubes
are additive Q = Q1 + Q2 + …
Flow equation, Q =
Q = A x v or flow (ml/min) = cross sectional area (cm^2) x velocity
CO = (MEMORIZE)
CO (ml/min)= HR (beat/min) X SV (ml)
Pulse pressure, PP = (MEMORIZE)
PP = SP - DP
PP is used in MAP equation
Turbulent flow is characterized by Reynolds number, Re =
Re = 2rvd/U
r = radius v= velocity d = density U = viscosity
Re>3000 = Turbulent
Re<2000 = Laminar
Re between 3000 & 2000 = transitional