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Formula Sheet: Fluids in Motion

Continuity Equation

Fundamental Principle

  • Conservation of Mass: For an incompressible fluid, mass flow rate must remain constant throughout a pipe or tube
  • Volume Flow Rate (Q): \[Q = A \times v\] where:
    • \(Q\) = volume flow rate (m³/s)
    • \(A\) = cross-sectional area (m²)
    • \(v\) = fluid velocity (m/s)

Continuity Equation

  • Standard Form: \[A_1 v_1 = A_2 v_2\] where subscripts 1 and 2 represent different points along the flow path
  • Important Relationship: As cross-sectional area decreases, fluid velocity increases (and vice versa)
  • Assumptions: Incompressible fluid, steady flow, single inlet and outlet

Bernoulli's Equation

Full Bernoulli Equation

  • Energy Conservation Form: \[P_1 + \frac{1}{2}\rho v_1^2 + \rho g h_1 = P_2 + \frac{1}{2}\rho v_2^2 + \rho g h_2\] where:
    • \(P\) = absolute pressure (Pa or N/m²)
    • \(\rho\) = fluid density (kg/m³)
    • \(v\) = fluid velocity (m/s)
    • \(g\) = gravitational acceleration (9.8 m/s²)
    • \(h\) = height above reference point (m)
  • Alternative Form: \[P + \frac{1}{2}\rho v^2 + \rho g h = \text{constant}\]

Energy Terms in Bernoulli's Equation

  • Pressure Energy: \(P\) = static pressure
  • Kinetic Energy per Unit Volume: \(\frac{1}{2}\rho v^2\) = dynamic pressure
  • Gravitational Potential Energy per Unit Volume: \(\rho g h\)
  • Note: All three terms have units of pressure (Pa)

Assumptions and Limitations

  • Fluid is incompressible (constant density)
  • Flow is steady (non-turbulent, laminar)
  • Flow is non-viscous (no internal friction/energy loss)
  • Flow occurs along a streamline

Special Applications of Bernoulli's Equation

Horizontal Flow (No Height Change)

  • When \(h_1 = h_2\): \[P_1 + \frac{1}{2}\rho v_1^2 = P_2 + \frac{1}{2}\rho v_2^2\]
  • Implication: As velocity increases, pressure decreases

Torricelli's Theorem (Efflux Speed)

  • Speed of fluid exiting a hole: \[v = \sqrt{2gh}\] where:
    • \(v\) = efflux velocity (m/s)
    • \(g\) = gravitational acceleration (9.8 m/s²)
    • \(h\) = depth of hole below fluid surface (m)
  • Derivation assumption: Large container (surface velocity ≈ 0), atmospheric pressure at surface and hole

Venturi Effect

  • Concept: Fluid pressure decreases in a constricted section of pipe where velocity increases
  • Combined with Continuity: Use \(A_1 v_1 = A_2 v_2\) with Bernoulli's equation to solve for pressure or velocity changes

Viscosity and Resistance to Flow

Dynamic Viscosity

  • Definition: Measure of a fluid's resistance to flow and internal friction
  • Symbol: \(\eta\) (eta)
  • Units: Pa·s or N·s/m² or kg/(m·s)
  • Temperature dependence: Viscosity of liquids decreases with increasing temperature; viscosity of gases increases with increasing temperature

Laminar vs. Turbulent Flow

  • Laminar Flow: Smooth, orderly flow in parallel layers; occurs at low velocities
  • Turbulent Flow: Chaotic, irregular flow with eddies; occurs at high velocities
  • Reynolds Number (Re): Dimensionless parameter predicting flow type \[Re = \frac{\rho v D}{\eta}\] where:
    • \(\rho\) = fluid density (kg/m³)
    • \(v\) = fluid velocity (m/s)
    • \(D\) = diameter of pipe (m)
    • \(\eta\) = dynamic viscosity (Pa·s)
  • Critical values: Re < 2000="" typically="" laminar;="" re=""> 4000 typically turbulent

Poiseuille's Law

Volume Flow Rate for Viscous Flow

  • Poiseuille's Equation: \[Q = \frac{\pi r^4 \Delta P}{8 \eta L}\] where:
    • \(Q\) = volume flow rate (m³/s)
    • \(r\) = radius of tube (m)
    • \(\Delta P\) = pressure difference between ends (Pa)
    • \(\eta\) = dynamic viscosity (Pa·s)
    • \(L\) = length of tube (m)
  • Key relationship: Flow rate is proportional to \(r^4\) (doubling radius increases flow 16-fold)
  • Assumptions: Laminar flow, incompressible Newtonian fluid, rigid cylindrical tube

Resistance to Flow

  • Hydraulic Resistance: \[R = \frac{8 \eta L}{\pi r^4}\]
  • Flow-Resistance Relationship: \[Q = \frac{\Delta P}{R}\] (analogous to Ohm's Law: \(I = V/R\))
  • Note: Resistance is inversely proportional to \(r^4\)

Series and Parallel Resistance

  • Resistances in Series: \[R_{total} = R_1 + R_2 + R_3 + ...\]
  • Resistances in Parallel: \[\frac{1}{R_{total}} = \frac{1}{R_1} + \frac{1}{R_2} + \frac{1}{R_3} + ...\]

Fluid Dynamics in Physiology

Blood Flow Applications

  • Mean Arterial Pressure (MAP): Average pressure during one cardiac cycle, approximately: \[MAP \approx \frac{P_{systolic} + 2P_{diastolic}}{3}\]
  • Cardiac Output (CO): \[CO = HR \times SV\] where:
    • \(CO\) = cardiac output (L/min)
    • \(HR\) = heart rate (beats/min)
    • \(SV\) = stroke volume (L/beat)

Vascular Resistance and Blood Pressure

  • Total Peripheral Resistance (TPR): \[TPR = \frac{\Delta P}{CO}\] where \(\Delta P\) is pressure difference across systemic circulation
  • Implication of Poiseuille's Law: Small changes in vessel radius (vasoconstriction/vasodilation) dramatically affect resistance and flow

Additional Flow Relationships

Mass Flow Rate

  • Definition: \[\dot{m} = \rho Q = \rho A v\] where:
    • \(\dot{m}\) = mass flow rate (kg/s)
    • \(\rho\) = fluid density (kg/m³)
    • \(Q\) = volume flow rate (m³/s)

Power in Fluid Flow

  • Power delivered by pressure: \[P_{power} = \Delta P \times Q\] where:
    • \(P_{power}\) = power (W or J/s)
    • \(\Delta P\) = pressure difference (Pa)
    • \(Q\) = volume flow rate (m³/s)

Important Conceptual Relationships

Pressure-Velocity Relationship

  • In horizontal flow: high velocity → low pressure (Bernoulli principle)
  • In horizontal flow: low velocity → high pressure
  • Examples: airplane wing lift, atomizer/sprayer function, Venturi meter

Area-Velocity Relationship

  • From continuity: small area → high velocity
  • From continuity: large area → low velocity
  • Example: blood flows fastest in aorta, slowest in capillaries (due to total cross-sectional area)

Radius-Flow Relationship

  • From Poiseuille's Law: Flow ∝ r4
  • Small decreases in radius cause dramatic decreases in flow
  • Clinical relevance: atherosclerosis, vasoconstriction effects

Common Problem-Solving Strategies

Using Continuity and Bernoulli Together

  1. Apply continuity equation to relate velocities at two points: \(A_1 v_1 = A_2 v_2\)
  2. Substitute into Bernoulli's equation to solve for unknown pressure or velocity
  3. Check units and physical reasonableness of answer

Identifying Appropriate Equation

  • Ideal fluid (non-viscous), energy conservation: Use Bernoulli's equation
  • Real fluid with viscosity, cylindrical tube: Use Poiseuille's Law
  • Volume or mass conservation: Use continuity equation
  • Hole in container: Use Torricelli's theorem
The document Formula Sheet: Fluids in Motion is a part of the MCAT Course Formula Sheets for MCAT.
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