Fluid Flow, Continuity, and Bernoulli’s Equation (4B) - MCAT Chemical and Physical Foundations of Biological Systems
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Using continuity, if a pipe narrows so that $A_2=\frac{1}{2}A_1$, what is $v_2$ in terms of $v_1$?
Using continuity, if a pipe narrows so that $A_2=\frac{1}{2}A_1$, what is $v_2$ in terms of $v_1$?
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$v_2=2v_1$. Continuity requires speed to double when area halves to maintain constant flow rate in incompressible flow.
$v_2=2v_1$. Continuity requires speed to double when area halves to maintain constant flow rate in incompressible flow.
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For horizontal flow, if speed increases from $v_1$ to $v_2$ with $v_2>v_1$, how does pressure change?
For horizontal flow, if speed increases from $v_1$ to $v_2$ with $v_2>v_1$, how does pressure change?
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$P_2<P_1$. Bernoulli’s principle shows that increased speed in horizontal flow reduces pressure to conserve energy.
$P_2<P_1$. Bernoulli’s principle shows that increased speed in horizontal flow reduces pressure to conserve energy.
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In a horizontal pipe, if $v_2=2v_1$, what is $P_1-P_2$ in terms of $\rho$ and $v_1$?
In a horizontal pipe, if $v_2=2v_1$, what is $P_1-P_2$ in terms of $\rho$ and $v_1$?
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$P_1-P_2=\frac{3}{2}\rho v_1^2$. From simplified Bernoulli’s equation, pressure drop equals the difference in dynamic pressures for $v_2=2v_1$.
$P_1-P_2=\frac{3}{2}\rho v_1^2$. From simplified Bernoulli’s equation, pressure drop equals the difference in dynamic pressures for $v_2=2v_1$.
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In a vertical pipe with equal speeds ($v_1=v_2$), what is $P_2-P_1$ if $h_2-h_1=\Delta h$?
In a vertical pipe with equal speeds ($v_1=v_2$), what is $P_2-P_1$ if $h_2-h_1=\Delta h$?
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$P_2-P_1=-\rho g\Delta h$. With equal speeds, Bernoulli’s equation shows pressure difference opposes gravitational potential change.
$P_2-P_1=-\rho g\Delta h$. With equal speeds, Bernoulli’s equation shows pressure difference opposes gravitational potential change.
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What is the definition of a streamline in fluid flow?
What is the definition of a streamline in fluid flow?
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A curve everywhere tangent to the local fluid velocity. A streamline traces the path where its direction matches the instantaneous velocity vector of the fluid particles.
A curve everywhere tangent to the local fluid velocity. A streamline traces the path where its direction matches the instantaneous velocity vector of the fluid particles.
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What is the definition of laminar flow in a pipe?
What is the definition of laminar flow in a pipe?
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Smooth, layered flow with minimal mixing between layers. Laminar flow features parallel layers sliding past each other with viscous forces dominating, preventing mixing.
Smooth, layered flow with minimal mixing between layers. Laminar flow features parallel layers sliding past each other with viscous forces dominating, preventing mixing.
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What is the definition of turbulent flow in a pipe?
What is the definition of turbulent flow in a pipe?
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Chaotic flow with eddies and significant mixing. Turbulent flow involves inertial forces dominating, leading to irregular motion and vortex formation.
Chaotic flow with eddies and significant mixing. Turbulent flow involves inertial forces dominating, leading to irregular motion and vortex formation.
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State the Reynolds number formula for flow in a cylindrical tube.
State the Reynolds number formula for flow in a cylindrical tube.
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$\text{Re}=\frac{\rho vD}{\mu}$. Reynolds number Re quantifies the ratio of inertial to viscous forces using density, speed, diameter, and viscosity.
$\text{Re}=\frac{\rho vD}{\mu}$. Reynolds number Re quantifies the ratio of inertial to viscous forces using density, speed, diameter, and viscosity.
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For pipe flow, which inequality indicates a strong tendency toward turbulence using Reynolds number?
For pipe flow, which inequality indicates a strong tendency toward turbulence using Reynolds number?
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$\text{Re}\gtrsim 2000$. In pipe flow, Re exceeding approximately 2000 indicates inertial forces overpower viscous damping, promoting turbulence.
$\text{Re}\gtrsim 2000$. In pipe flow, Re exceeding approximately 2000 indicates inertial forces overpower viscous damping, promoting turbulence.
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State Poiseuille’s law for laminar flow rate $Q$ through a cylindrical tube of radius $r$ and length $L$.
State Poiseuille’s law for laminar flow rate $Q$ through a cylindrical tube of radius $r$ and length $L$.
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$Q=\frac{\pi r^4\Delta P}{8\mu L}$. Poiseuille’s law derives from viscous flow assumptions, showing flow rate proportional to pressure gradient and radius to the fourth power.
$Q=\frac{\pi r^4\Delta P}{8\mu L}$. Poiseuille’s law derives from viscous flow assumptions, showing flow rate proportional to pressure gradient and radius to the fourth power.
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What is the definition of volumetric flow rate $Q$ for a fluid?
What is the definition of volumetric flow rate $Q$ for a fluid?
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$Q=\frac{dV}{dt}$. Volumetric flow rate $Q$ measures the volume of fluid $dV$ passing through a cross-section per unit time $dt$.
$Q=\frac{dV}{dt}$. Volumetric flow rate $Q$ measures the volume of fluid $dV$ passing through a cross-section per unit time $dt$.
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State the continuity equation relating flow rate, area, and speed for steady incompressible flow.
State the continuity equation relating flow rate, area, and speed for steady incompressible flow.
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$Q=Av$. For steady incompressible flow, volumetric flow rate $Q$ equals cross-sectional area $A$ times average fluid speed $v$.
$Q=Av$. For steady incompressible flow, volumetric flow rate $Q$ equals cross-sectional area $A$ times average fluid speed $v$.
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What is the continuity relationship between two points in an incompressible fluid ($1$ and $2$)?
What is the continuity relationship between two points in an incompressible fluid ($1$ and $2$)?
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$A_1v_1=A_2v_2$. Continuity for incompressible fluids ensures constant flow rate, so the product of area and speed remains equal at different points.
$A_1v_1=A_2v_2$. Continuity for incompressible fluids ensures constant flow rate, so the product of area and speed remains equal at different points.
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Identify the correct unit for volumetric flow rate $Q$ in SI units.
Identify the correct unit for volumetric flow rate $Q$ in SI units.
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$\text{m}^3!!/\text{s}$. In SI units, volumetric flow rate $Q$ is expressed as cubic meters per second, reflecting volume over time.
$\text{m}^3!!/\text{s}$. In SI units, volumetric flow rate $Q$ is expressed as cubic meters per second, reflecting volume over time.
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What is the definition of mass flow rate $\dot{m}$ in terms of density and $Q$?
What is the definition of mass flow rate $\dot{m}$ in terms of density and $Q$?
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$\dot{m}=\rho Q$. Mass flow rate $\dot{m}$ is the product of fluid density $\rho$ and volumetric flow rate $Q$, giving mass per unit time.
$\dot{m}=\rho Q$. Mass flow rate $\dot{m}$ is the product of fluid density $\rho$ and volumetric flow rate $Q$, giving mass per unit time.
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State the relationship between gauge pressure $P_g$ and absolute pressure $P_{abs}$.
State the relationship between gauge pressure $P_g$ and absolute pressure $P_{abs}$.
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$P_{abs}=P_g+P_{atm}$. Absolute pressure $P_{abs}$ includes atmospheric pressure $P_{atm}$ added to gauge pressure $P_g$, accounting for total pressure.
$P_{abs}=P_g+P_{atm}$. Absolute pressure $P_{abs}$ includes atmospheric pressure $P_{atm}$ added to gauge pressure $P_g$, accounting for total pressure.
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State Bernoulli’s equation for steady, incompressible, nonviscous flow along a streamline.
State Bernoulli’s equation for steady, incompressible, nonviscous flow along a streamline.
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$P+\frac{1}{2}\rho v^2+\rho gh=\text{constant}$. Bernoulli’s equation conserves energy per unit volume along a streamline, summing static, dynamic, and gravitational terms.
$P+\frac{1}{2}\rho v^2+\rho gh=\text{constant}$. Bernoulli’s equation conserves energy per unit volume along a streamline, summing static, dynamic, and gravitational terms.
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Write Bernoulli’s equation explicitly between two points ($1$ and $2$) on a streamline.
Write Bernoulli’s equation explicitly between two points ($1$ and $2$) on a streamline.
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$P_1+\frac{1}{2}\rho v_1^2+\rho gh_1=P_2+\frac{1}{2}\rho v_2^2+\rho gh_2$. Bernoulli’s equation equates the sum of pressures and energies at two points on a streamline for conservation in ideal flow.
$P_1+\frac{1}{2}\rho v_1^2+\rho gh_1=P_2+\frac{1}{2}\rho v_2^2+\rho gh_2$. Bernoulli’s equation equates the sum of pressures and energies at two points on a streamline for conservation in ideal flow.
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What is the definition of dynamic pressure in Bernoulli’s equation?
What is the definition of dynamic pressure in Bernoulli’s equation?
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$\frac{1}{2}\rho v^2$. Dynamic pressure represents the kinetic energy per unit volume of the moving fluid in Bernoulli’s equation.
$\frac{1}{2}\rho v^2$. Dynamic pressure represents the kinetic energy per unit volume of the moving fluid in Bernoulli’s equation.
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What is the definition of hydrostatic (gravitational) pressure term in Bernoulli’s equation?
What is the definition of hydrostatic (gravitational) pressure term in Bernoulli’s equation?
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$\rho gh$. Hydrostatic pressure arises from gravitational potential energy per unit volume at height $h$ in a fluid of density $\rho$.
$\rho gh$. Hydrostatic pressure arises from gravitational potential energy per unit volume at height $h$ in a fluid of density $\rho$.
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Which condition must hold for the continuity form $A_1v_1=A_2v_2$ to be valid?
Which condition must hold for the continuity form $A_1v_1=A_2v_2$ to be valid?
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Steady, incompressible flow. The continuity equation $A_1v_1=A_2v_2$ assumes steady flow with constant density, ensuring mass conservation.
Steady, incompressible flow. The continuity equation $A_1v_1=A_2v_2$ assumes steady flow with constant density, ensuring mass conservation.
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Which condition must hold for Bernoulli’s equation to apply in its simplest form?
Which condition must hold for Bernoulli’s equation to apply in its simplest form?
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Steady, incompressible, nonviscous flow on a streamline. Bernoulli’s equation in simplest form requires no viscosity, constant density, steady flow, and evaluation along a streamline.
Steady, incompressible, nonviscous flow on a streamline. Bernoulli’s equation in simplest form requires no viscosity, constant density, steady flow, and evaluation along a streamline.
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Identify the correct expression for average speed $v$ in a tube given $Q$ and cross-sectional area $A$.
Identify the correct expression for average speed $v$ in a tube given $Q$ and cross-sectional area $A$.
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$v=\frac{Q}{A}$. Average fluid speed $v$ derives from rearranging the flow rate equation $Q=Av$ for a given cross-section.
$v=\frac{Q}{A}$. Average fluid speed $v$ derives from rearranging the flow rate equation $Q=Av$ for a given cross-section.
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For a horizontal pipe, what does Bernoulli’s equation reduce to between points $1$ and $2$?
For a horizontal pipe, what does Bernoulli’s equation reduce to between points $1$ and $2$?
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$P_1+\frac{1}{2}\rho v_1^2=P_2+\frac{1}{2}\rho v_2^2$. In horizontal flow, gravitational terms cancel in Bernoulli’s equation, leaving static and dynamic pressure balance.
$P_1+\frac{1}{2}\rho v_1^2=P_2+\frac{1}{2}\rho v_2^2$. In horizontal flow, gravitational terms cancel in Bernoulli’s equation, leaving static and dynamic pressure balance.
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Using continuity, if $A_2=3A_1$, what is $v_2$ in terms of $v_1$ for incompressible flow?
Using continuity, if $A_2=3A_1$, what is $v_2$ in terms of $v_1$ for incompressible flow?
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$v_2=\frac{1}{3}v_1$. Continuity dictates that speed decreases inversely with area increase to conserve volume flow rate.
$v_2=\frac{1}{3}v_1$. Continuity dictates that speed decreases inversely with area increase to conserve volume flow rate.
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