Blood Vessel Formulas.

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Presentation transcript:

Blood Vessel Formulas

Mathematical Analysis of the Circulatory System Discussion of Pressure Discussion of Pressure in a pipe without an external compression device (pressure in the blood vessels without the heart) known as “Mean Circulatory Filling Pressure”. Discuss unstressed and stressed blood volume Discuss pressure in blood vessels with heart compression Discuss Flow – velocity of flow versus rate of flow Discuss Resistance – resistance in pipes arranged in series versus those arranged in parallel Total Peripheral Resistance Examine Diffusion Formula Examine Capacitance (Compliance) Formula Examine the Mean Arterial Pressure Formulas Wall Tension

Pressure Pulling or pushing force Volume of gas or liquid Density of gas or liquid Pressure = Volume/1 X particles/volume X force/particle Pressure = force Mercury is 13.6 times more dense than water, so the same volume of mercury can exert far more pressure than water.

Mean Circulatory Filling Pressure The pressure in your blood vessels without a heart. The pressure depends on (1) volume of blood in your blood vessels and (2) the amount of vasodilation or constriction. The average value is 7 mmHg The volume and/or vasoconstriction – the pressure goes up and vice versa.

Stressed and Unstressed Blood Volume Unstressed Blood Volume is the volume in the blood vessels before there is enough to stretch out the blood vessels walls. When there begins to be enough in the blood vessels to stretch out the blood vessels walls, that amount of blood that does that is the stressed blood volume.

Adding the Heart Pressure Total = Compression Pressure of the Heart + MCFP In order to stand up, you need a 60mmHg pressure, if the MCFP is even 12 mmHg, you still need a working heart. Assume this container to be The blood vessels. The pressure in this Container is the “Mean Circulatory Filling Pressure.” It has an average Pressure of 7mmHg, But can raise or lower Based on how much fluid you put in or how much to enlarge the tank diameter or decrease it; that would symbolize vasodilation and vasoconstriction. When you add the pressure Of the heart it would be the Mean circulatory filling pressure Plus the heart compression Pressure.

Formulas of importance Flow = ∆P/ R, ∆P is the change in pressure from one area to another (P1 – P2) – in the direction of flow, R is the resistance (Note: pressure drops off as a fluid or gas passes further down the pipe – thus the pressure in proximal area 1 (P1) is higher than the pressure is distal area 2. The more pressure drop off the more the flow. Also, the less the resistance the better the flow. Rate of Flow = amount of gas or liquid/time (example ml/min) Velocity of flow = amount of gas or liquid/time/cross sectional area (another way of looking at it is Vf = rate of flow/cross sectional area) example of velocity of flow ml. /min per cm2 Note: Area of a circle (like the inside of a vessel ) = equals pi (π) times the radius squared (π⋅r2), example ml. /min per cm2 Flow formula derived Ohm’s Law

Rate of Flow versus Velocity of Flow The rate of flow is how much per some unit time, for example ml./minute. The velocity of flow is how much per some unit time per cross sectional area.

Let’s think of it this way Let’s compare a solid object to continuous substances like gases and liquids. A solid object has a discrete structure like a car; it has a definite beginning and end. Gases and liquids have a more fuzzy begin and end. A car traveling 25 miles/hour. It says how much distance (area), the time and how many – one car. A liquid flows at 25 ml./minute. It says how much (25 ml.), time, but no area. This is the rate of flow. If I said the liquid flows at 25 ml./minute/meter squared, that would be the velocity of flow. So gases and liquids have two measurements of flow: rate of flow and velocity of flow.

Formulas of Importance Resistance –a force of impedance (holding back) R = 8ηL/πR4 , η is viscosity of the gas or liquid, L is the length of the vessel, and R is the radius raised to the 4th power Summation (∑) of Resistances – adding up the resistors in flow arrangement a series arrange Resistors in series – one resistor in front of another ∑ = R1 + R2 + R3 + …… Resistors in parallel – a pipe leads into a branching set of pipes ∑ = 1/R1 + 1/R2 + 1/R3 +.. Note: resistors in parallel give less total resistance than those in series (think of the capillary arrangement)

Resistance Resistance –a force of impedance (holding back) R = 8ηL/πR4 , η is viscosity of the gas or liquid L is the length of the vessel R is the radius raised to the 4th power π – a constant

Adding up Resistances Summation (∑) of resistances depends on are the resistors in series or parallel. Resistors in series – one resistor in front of another ∑ = R1 + R2 + R3 + …… Resistors in parallel – a pipe leads into a branching set of pipes ∑ = 1/R1 + 1/R2 + 1/R3 +.. Note: resistors in parallel give less total resistance than those in series (think of the capillary arrangement)

Total Peripheral Resistance (Systemic Vascular Resistance) The TPR (SVR) is the summation (∑ ) of all the resistors in the systemic (Left Ventricle – to Right Atrium) circulation. Some of the blood vessel resistors are in series (R1 + R2 + R3 + ……) and some are in parallel (1/R1 + 1/R2 + 1/R3 )– thus the two different formulas must be used. Since R is raised to 4th power it numerically is the most significant contributor to Total Peripheral Resistance – thus vasoconstriction and vasodilation are the most important contributors to TPR. Alternate calculations are Total Pulmonary Resistance which is resistance in the pulmonary circulation – as well as other organ and circulatory resistances can be calculated

Formulas of Importance Diffusion – net movement of certain particles from a region of high concentration of those certain particles to region of low concentration of those certain particles D = A x Dc /t (Co – Ci) A is the area of the membrane being diffused through, Dc is the diffusion coefficient, t- is the thickness of the membrane being diffused through, Co – Ci is the concentration difference between the o (outside) and I (inside) of the container The diffusion coefficient = solubility coefficient divided by the square root of the molecular weight of the substance diffusing (this applies more to gases) Analysis- the greater the area and/or diffusion coefficient – the faster the rate of diffusion. The more the concentration difference the faster the rate of diffusion. However, the thicker the membrane to diffuse through the slower the rate of diffusion.

Formulas of Importance Capacitance (Compliance) C – is the ease at which a container can stretch to accommodate increased volumes of gases or liquids. C = ∆V/∆P, ∆P is change in pressure, and ∆V is change in volume The more volume change without a change in pressure (due to compression of atoms and molecules in a minimally stretchable container) the greater the capacitance (compliance) Thus a balloon would have greater capacitance (compliance) that a leather container.

Laminar Flow Versus Turbulent Flow Laminar flow, sometimes known as streamline flow, occurs when a fluid flows in parallel layers, with no disruption between the layers. It is the opposite of turbulent flow. In nonscientific terms laminar flow is "smooth," while turbulent flow is "rough."

Laminar Flow is a quiet smooth flow through blood vessels – whereas turbulent flow makes a noise as it flows – the more turbulent the flow the louder the noise. Turbulent flow produces murmur like sounds in the heart. A Bruit is the unusual sound that blood makes when it rushes past an obstruction (called turbulent flow) in an artery when the sound is auscultated with the bell portion of a stethoscope. A related term is "vascular murmur", which should not be confused with a heart murmur.

Determining if flow is Laminar versus Turbulent The Reynolds number is used to determine whether a flow will be laminar or turbulent. Reynolds number (Re) is the ratio of inertial forces to viscous forces and is given by the formula: Re = ρVD/μ where ρ = density of the fluid, V = velocity, D = pipe diameter, and μ = fluid viscosity. If Re is high (>2100), inertial forces dominate viscous forces and the flow is turbulent; if Re number is low (<1100), viscous forces dominate and the flow is laminar.

Mean Arterial Pressure It is defined as the average arterial pressure during a single cardiac cycle. MAP (SYSTEMIC) = CO X TPR (SVR) MAP (SYSTEMIC) is the average pressure in the systemic circulation (Left Ventricle to Right Atrium). Thus MAP (pulmonic) can be calculated also as well as other circulations. CO is the cardiac output = heart rate x stroke volume (stroke volume is End Diastolic Volume – End Systolic Volume) TPR (SVR) is the total resistance in the systemic circulation

MAP (SYSTEMIC) = CO X TPR (SVR) This formula is an excellent one to use to understand pressures in the blood vessels. It can explain hypertensive pressures, normotensive pressures and hypotensive pressures. However, it cannot be actually calculated in that the TPR cannot be calculated. TPR in involves calculating the radius of the blood vessels at each millimeter along the circulation – the human body has approximately 60,000 miles of blood vessels – thus this is impossible to calculate. The algebraic formula used to calculate MAP is MAP = DBP + 1/3 (SBP – DBP) DBP is the Diastolic Blood Pressure, and SBP is the Systolic Blood Pressure SBP – DBP is the Pulse Pressure

MAP = DBP + 1/3 (SBP – DBP) Systolic Blood Pressure – occurs during Ejection Contraction Time The Diastolic Blood Pressure has more weight (significance) in this formula – because during one cardiac cycle there is more time spent in diastole in the blood vessels than is systole. The actual way MAP is calculated by the computer (arterial line) is using differential Calculus. Differential calculus exactly calculates the area under a curve.

Blood Vessel Wall Tension Tension = Pressure inside vessel x r/ 2 r is radius of the vessel Interpretation: For a given blood pressure, increasing the radius of the blood vessel leads to a linear increase in tension. This implies that large arteries must have thicker walls than small arteries in order to withstand the level of tension.