100 MCQ's Fluid Mechanics Welcome to the ultimate Fluid Mechanics Quiz — designed exclusively for mechanical engineers, students, and aspirants who want to master the science of fluids in motion and at rest.This quiz blends learning with fun, helping you strengthen your fundamentals through 100 thoughtfully selected multiple-choice questions. Whether you’re preparing for exams or brushing up on concepts, this is where your flow of knowledge begins! 1 / 100 The flow rate through a Venturi meter is proportional to Reciprocal of pressure difference √(Pressure difference) Pressure difference Square of pressure difference According to Bernoulli’s equation, discharge varies as the square root of the pressure difference. 2 / 100 Coefficient of discharge accounts for Energy losses and contraction Only energy losses Only contraction None of these It includes both energy losses and contraction effects, correcting theoretical flow rate. 3 / 100 The discharge through a V-notch varies as √h h^2 h^(3/2) h^(5/2) For a V-notch, discharge is proportional to h^(5/2), providing higher sensitivity for small flows. 4 / 100 A weir is used for measuring discharge in Pipes Nozzles Open channels Closed conduits Weirs are barriers across open channels that allow flow measurement by head variation. 5 / 100 The discharge through a notch or weir varies as Head Square root of head Square of head Cube of head Flow rate is proportional to √h because it follows Bernoulli’s principle. 6 / 100 A Venturi meter gives more accurate results than an orifice meter because Flow separation is more Velocity is less Turbulence is high Energy losses are less Smooth flow and gradual contraction in a Venturi meter minimize energy losses. 7 / 100 In a flow-measuring device, if the differential head increases, discharge Increases Decreases Remains constant First increases then decreases Higher pressure difference means greater velocity and thus greater discharge. 8 / 100 The coefficient of velocity for an orifice is generally 0.98 0.65 0.70 0.85 Coefficient of velocity indicates actual to theoretical velocity ratio, usually about 0.98. 9 / 100 A rectangular notch is used when Velocity is low Flow is laminar Discharge is large Discharge is small Rectangular notches are best for measuring large discharges accurately. 10 / 100 The discharge coefficient of an orifice meter depends on Pipe diameter Pipe length Pipe material Reynolds number Discharge coefficient changes slightly with Reynolds number due to viscous effects. 11 / 100 The flow rate through a nozzle is maximum when the exit pressure equals Critical pressure Atmospheric pressure Zero pressure Gauge pressure Flow becomes choked at critical pressure, giving maximum discharge 12 / 100 The Pitot-static tube measures Velocity of flow Pressure difference Head loss Discharge It measures the dynamic pressure to calculate velocity using Bernoulli’s principle 13 / 100 The head loss in an Orifice meter is Equal to Venturi meter Negligible Less than Venturi meter More than Venturi meter Orifice meters cause greater head loss due to sharp-edged plates and flow separation 14 / 100 A V-notch is generally used for measuring Compressible flow Small discharges Large discharges High-pressure flow V-notches provide accurate measurement for small discharges because of their sensitivity. 15 / 100 The device used for measuring discharge in open channels is Notch Venturi meter Pitot tube Orifice Notches (like rectangular or V-notch) are used to measure flow rates in open channels. 16 / 100 The coefficient of discharge for a Venturi meter is approximately 0.55 0.65 0.75 0.98 The Venturi meter has a high coefficient of discharge (~0.98) due to low energy loss. 17 / 100 Which instrument measures flow velocity directly? Orifice meter Venturi meter Manometer Pitot tube A Pitot tube measures the stagnation and static pressure difference to directly find the flow velocity. 18 / 100 The discharge through an Orifice meter is measured by observing Velocity of flow Pressure difference across the orifice Area of pipe Head loss The flow rate in an Orifice meter is calculated using the pressure drop across the orifice plate. 19 / 100 In a Venturi meter, the pressure is lowest at the Inlet Outlet Throat Any section Velocity is maximum at the throat, so pressure is minimum due to energy conservation. 20 / 100 The Venturi meter works on which principle? Bernoulli’s principle Continuity equation Pascal’s law Newton’s law The Venturi meter measures flow using pressure difference between the throat and inlet, based on Bernoulli’s theorem 21 / 100 The total energy line lies Coinciding with the pipe axis At atmospheric level Above the hydraulic gradient line Below the hydraulic gradient line The total energy line includes both pressure and velocity heads, so it’s always above the hydraulic gradient. 22 / 100 In a horizontal pipe, the total energy line and hydraulic gradient line are Perpendicular Parallel Intersecting Coinciding For steady flow in a horizontal pipe, energy losses are uniform, keeping lines parallel. 23 / 100 The discharge through a venturi meter increases when Pipe diameter decreases Fluid density decreases Flow becomes turbulent Pressure difference increases Higher pressure difference means higher velocity and hence greater flow rate. 24 / 100 In laminar flow, the head loss is proportional to Velocity Velocity squared Pressure Area In laminar regime, head loss ∝ velocity, while in turbulent regime it ∝ velocity². 25 / 100 The Hagen–Poiseuille equation applies to Laminar flow through circular pipes Turbulent flow Flow over flat plate Flow through nozzles It defines relation between pressure drop and flow rate for viscous, laminar flow in pipes. 26 / 100 The discharge through an orifice is given by a × h Cd × √(2gh) a × √(2gh) Cd × a × √(2gh) The actual discharge depends on the orifice area, head, and coefficient of discharge. 27 / 100 The flow in a pipe is turbulent if Reynolds number is Greater than 4000 Less than 2000 Equal to 2000 Between 0 and 1000 At high Reynolds numbers, inertial forces dominate viscous forces, creating turbulence. 28 / 100 Flow separation occurs when Viscosity becomes zero Adverse pressure gradient causes reversal of flow Velocity increases suddenly Pressure is constant Flow separates when the fluid decelerates against an increasing pressure region, leading to turbulence. 29 / 100 In a nozzle, the velocity of fluid Decreases as pressure decreases Remains constant Becomes zero Increases as pressure decreases According to Bernoulli’s principle, as pressure energy drops, velocity energy rises 30 / 100 The value of coefficient of discharge for a venturi meter generally lies between 0.7 to 0.8 1.0 to 1.2 0.95 to 0.99 0.5 to 0.6 Venturi meters have high efficiency with minimal losses, giving Cd values close to 1.0. 31 / 100 The coefficient of discharge is the ratio of Actual discharge to theoretical discharge Theoretical discharge to actual discharge Velocity head to total head Measured head to velocity head It corrects for energy losses and gives the real discharge from theoretical calculations. 32 / 100 The head loss due to friction in pipes is given by Archimedes’ principle Darcy–Weisbach equation Bernoulli’s equation Pascal’s law Darcy–Weisbach equation relates head loss to pipe length, diameter, flow velocity, and friction factor. 33 / 100 The loss of energy due to fluid friction in a pipe is called Energy drop Pressure head Head loss Velocity loss When fluid flows through a pipe, friction converts part of mechanical energy into heat, causing head loss. 34 / 100 The flow through a nozzle is an example of Rotational flow Uniform flow Steady flow Unsteady flow The velocity and flow rate remain constant with time — hence steady flow. 35 / 100 In a horizontal venturi meter, pressure is Maximum at inlet and minimum at throat Minimum at inlet and maximum at throat Constant throughout Zero at throat As velocity increases at the throat, pressure decreases — a direct result of Bernoulli’s principle. 36 / 100 The device based on Bernoulli’s principle used to measure flow rate is Orifice plate Barometer Venturimeter Manometer Venturimeter uses pressure difference between two points in a pipe to measure discharge. 37 / 100 Bernoulli’s equation holds good for Turbulent flow Viscous flow Compressible flow Inviscid, incompressible, steady flow along a streamline It assumes fluid is non-viscous, incompressible, and flowing steadily without energy losses. 38 / 100 The total head in a flowing fluid is equal to Pressure head + Velocity head + Potential head Pressure head + Density head Velocity head + Energy head Pressure head only Total head is the sum of pressure energy, kinetic energy, and potential energy per unit weight. 39 / 100 In Bernoulli’s equation, head due to pressure is represented as V²/2g z pV p/ρg The term p/ρg represents the pressure head or energy per unit weight due to pressure. 40 / 100 Bernoulli’s equation is based on the principle of Conservation of energy Conservation of mass Conservation of momentum Conservation of volume Bernoulli’s theorem states that the total energy (pressure + kinetic + potential) of a fluid remains constant along a streamline. 41 / 100 The streamline and equipotential lines Intersect at random angles Are parallel Coincide Are always perpendicular to each other Streamlines show flow direction; equipotential lines show constant potential — hence, they intersect orthogonally. 42 / 100 The continuity equation is derived from Law of conservation of mass Law of conservation of energy Bernoulli’s equation Pascal’s law Continuity ensures that mass flow rate into a control volume equals mass flow rate out. 43 / 100 The velocity at a stagnation point is Zero Maximum Equal to free stream velocity Infinity At stagnation points, kinetic energy converts fully into pressure energy — velocity becomes zero. 44 / 100 The unit of discharge is m²/s m/s kg/s m³/s Discharge or flow rate measures volume of fluid passing per second — hence cubic meter per second. 45 / 100 If velocity potential φ and stream function ψ satisfy Laplace equation, the flow is Rotational Compressible Irrotational and incompressible Steady If both satisfy Laplace’s equation, it indicates potential flow that is both irrotational and incompressible. 46 / 100 Stream function exists for Compressible flow Steady flow only Irrotational flow only Incompressible flow Stream function is defined for 2D incompressible flow; its contours represent streamlines. 47 / 100 Turbulent flow occurs when Reynolds number > 4000 Reynolds number < 2000 Velocity is very low Pressure is constant When inertial forces dominate over viscous forces, flow becomes chaotic — that’s turbulence. 48 / 100 The type of flow in which adjacent layers of fluid glide smoothly over one another is Laminar flow Turbulent flow Steady flow Unsteady flow In laminar flow, there’s no mixing between layers — they move in smooth, orderly paths. 49 / 100 The path traced by a fluid particle over a period of time is known as Path line Streamline Streak line Timeline Pathline represents the actual trajectory that a single particle follows in motion. 50 / 100 In a rotational flow, the velocity potential Exists everywhere Is equal to stream function Is constant Does not exist Velocity potential is valid only for irrotational flows — rotational flows do not satisfy its conditions. 51 / 100 The flow in which velocity at a point changes with time is called Unsteady flow Steady flow Uniform flow Laminar flow In unsteady flow, the fluid velocity or other properties change over time at a fixed point. 52 / 100 The flow in a pipe is said to be laminar if Reynolds number is Less than 2000 Between 2000 and 4000 More than 4000 Exactly 4000 Laminar flow occurs when viscous forces dominate, keeping fluid layers smooth and parallel. 53 / 100 Stream function remains constant along A pathline An equipotential line A vortex line A streamline The stream function defines streamlines — its constant value represents a streamline. 54 / 100 The velocity potential function is applicable for Turbulent flow Irrotational flow Rotational flow Laminar flow Velocity potential exists only for irrotational flows, where fluid elements do not rotate about their axis. 55 / 100 The equation of continuity for an incompressible fluid is A₁V₁ = A₂V₂ A₁/V₁ = A₂/V₂ A₁V₁² = A₂V₂² A₁V₁ + A₂V₂ = 0 For incompressible flow, the product of area and velocity remains constant throughout the flow. 56 / 100 The continuity equation is based on the principle of Conservation of energy Conservation of momentum Conservation of volume Conservation of mass The continuity equation ensures the mass entering and leaving a control volume remains equal. 57 / 100 Flow in which the velocity is same at every point in a given section is called Uniform flow Non-uniform flow Steady flow Laminar flow In uniform flow, velocity magnitude and direction remain same along the length of flow. 58 / 100 If the velocity at a point in a fluid does not change with time, the flow is Uniform Non-uniform Steady Unsteady Steady flow means fluid properties like velocity remain constant with respect to time at a given point. 59 / 100 A streamline is a line Perpendicular to the velocity vector Tangent to the velocity vector at every point Parallel to the pressure gradient Coinciding with the flow path only at the inlet In steady flow, streamlines show the direction of fluid particles at every point in time. 60 / 100 The branch of fluid mechanics which deals with the motion of fluids without considering the forces causing motion is called Kinematics Hydraulics Dynamics Statics Fluid kinematics focuses only on describing motion — velocity, acceleration, and flow type — not the forces behind them. 61 / 100 A piezometer is used for measuring Pressure head of fluid Velocity of fluid Flow rate Temperature A piezometer is a simple vertical tube that indicates the pressure head at a point in fluid. 62 / 100 The buoyant force on a submerged body equals Weight of fluid displaced Weight of body Pressure difference Mass of fluid displaced Archimedes’ principle defines buoyant force equal to the displaced fluid’s weight. 63 / 100 The pressure in a liquid increases with Temperature Surface tension Depth Viscosity Deeper points in a fluid bear more pressure due to the weight of the liquid above. 64 / 100 A fluid at rest cannot sustain Compressive stress Tensile stress Shear stress Normal stress A static fluid only resists normal stresses; any shear causes motion. 65 / 100 A differential manometer measures Absolute pressure Atmospheric pressure Gauge pressure Difference of pressure between two points It shows pressure difference by comparing the heights of liquid columns in both limbs. 66 / 100 In a floating body, if the metacentric height is positive, the equilibrium is Stable Unstable Neutral None Positive metacentric height ensures the body returns to equilibrium after small tilts. 67 / 100 The centre of pressure for an inclined plane surface lies Below the centroid Above the centroid At the centroid At free surface Pressure increases with depth, so the resultant acts below the centroid. 68 / 100 The pressure intensity at the bottom of a tank filled with liquid depends on Viscosity of liquid Shape of tank Area of tank Depth and density of liquid Pressure at depth h = ρgh, independent of shape or area of tank. 69 / 100 The principle of buoyancy was given by Newton Archimedes Bernoulli Pascal Archimedes’ principle states that a body immersed in fluid experiences an upward force equal to the weight of displaced fluid. 70 / 100 The buoyant force on a body immersed in fluid acts through Centre of buoyancy Centre of gravity Centroid Centre of pressure The centre of buoyancy is the centroid of the displaced volume of fluid. 71 / 100 The pressure difference measured by a U-tube manometer depends on Density difference of the fluids Area of the tube Viscosity Temperature The pressure difference equals the product of height difference and density difference. 72 / 100 The total pressure on a plane surface submerged in a liquid acts Horizontally At an angle Parallel to the surface Perpendicular to the surface Hydrostatic pressure always acts normal to the surface. 73 / 100 The point where the total pressure acts on a submerged surface is called Neutral point Centre of pressure Centroid Centre of buoyancy Centre of pressure is the point of action of the resultant hydrostatic force on a surface. 74 / 100 A barometer measures Gauge pressure Vacuum pressure Absolute pressure of gas Atmospheric pressure A barometer measures atmospheric pressure using a column of mercury. 75 / 100 The pressure head is expressed as Density / Pressure Pressure × Density g / Pressure Pressure / (Density × g) Pressure head converts pressure into an equivalent column height of fluid. 76 / 100 A device used for measuring small pressure differences between two points is called Barometer Pressure gauge Venturi meter Manometer Manometers use a column of liquid to measure small pressure differences with high accuracy. 77 / 100 The absolute pressure is equal to Gauge pressure + Atmospheric pressure Atmospheric pressure − Gauge pressure Vacuum pressure + Gauge pressure None of the above Absolute pressure measures total pressure relative to perfect vacuum. 78 / 100 The unit of pressure in SI system is Bar atm Newton Pascal Pressure = Force/Area, and its SI unit is Pascal (Pa), equivalent to N/m². 79 / 100 The pressure at any point in a liquid at rest acts Equally in all directions Only vertically Only horizontally At an angle In a fluid at rest, the pressure acts equally in all directions, as stated by Pascal’s Law. 80 / 100 The pressure at a point in a static fluid increases with Depth of fluid Density of fluid Viscosity of fluid Temperature of fluid Pressure in a static fluid increases linearly with depth due to the weight of the fluid above the point. 81 / 100 The phenomenon of a liquid rising or falling in a narrow tube is called: Capillarity Viscosity Fluidity Adhesion Capillary action occurs due to the combined effect of surface tension and adhesive forces. 82 / 100 The unit of surface tension in SI system is: N/m N·s/m² kg/m³ m²/s Surface tension is the force per unit length acting along the surface of a liquid. 83 / 100 A fluid that obeys Newton’s law of viscosity is called: Newtonian fluid Ideal fluid Non-Newtonian fluid Compressible fluid Newtonian fluids have a linear relationship between shear stress and velocity gradient. 84 / 100 The ratio of absolute viscosity to kinematic viscosity gives: Density Surface tension Compressibility Fluidity Kinematic viscosity = Dynamic viscosity / Density, hence rearranging gives density. 85 / 100 The fluid property that resists the relative motion between adjacent layers is: Adhesion Viscosity Surface tension Elasticity Viscosity represents internal friction between fluid layers moving at different velocities. 86 / 100 The force of adhesion is between: Two liquid layers Liquid and gas Solid and solid Liquid and solid Adhesion occurs when a liquid sticks to a solid surface — it causes wetting behavior. 87 / 100 Which fluid property defines its ability to transmit pressure equally in all directions? Density Surface tension Viscosity Incompressibility A truly incompressible fluid can transmit pressure equally throughout its volume (Pascal’s Law). 88 / 100 Bernoulli’s equation is derived from the law of: Conservation of pressure Conservation of energy Conservation of mass Conservation of momentum Bernoulli’s principle relates pressure, velocity, and elevation for incompressible flow using energy conservation. 89 / 100 Continuity equation is based on the principle of: Conservation of mass Conservation of momentum Conservation of energy Conservation of volume The continuity equation states that mass entering and leaving a control volume must remain constant. 90 / 100 The pressure at a point in a static fluid acts: Vertically downward Horizontally only Equally in all directions Normal to the boundary only In a static fluid, pressure is isotropic — acting equally in all directions. 91 / 100 A fluid that has no viscosity is known as: Non-Newtonian fluid Newtonian fluid Real fluid Ideal fluid An ideal fluid is a simplified concept used in theoretical analysis to neglect viscosity effects. 92 / 100 The SI unit of dynamic viscosity is: N·s/m² kg/m³ m²/s Pa/m Dynamic viscosity quantifies internal resistance to flow, with its SI unit as N·s/m² (or Pa·s). 93 / 100 The ratio of dynamic viscosity to density is called: Specific gravity Kinematic viscosity Surface tension Fluidity Kinematic viscosity relates the viscous forces to the fluid’s inertia and is expressed in m²/s. 94 / 100 Which property of fluid changes with temperature most significantly? Viscosity Density Specific weight Surface tension Viscosity decreases with an increase in temperature for liquids, making flow easier. 95 / 100 The mass of a fluid per unit volume is called: Density Specific weight Surface tension Viscosity Surface tension acts along the interface between liquid and air, causing capillary rise or depression. 96 / 100 Which fluid property is responsible for the rise of liquid in a capillary tube? Viscosity Surface tension Density Specific weight Surface tension acts along the interface between liquid and air, causing capillary rise or depression. 97 / 100 Which of the following is a dimensionless quantity? Dynamic viscosity Kinematic viscosity Density Specific gravity Specific gravity is a pure ratio of densities, so it has no units. 98 / 100 Which of the following statements is true for an ideal fluid? It can be compressed easily It cannot flow It has viscosity but no density It is incompressible and has no viscosity An ideal fluid is theoretical — it cannot be compressed and has zero viscosity for simplified analysis. 99 / 100 The ratio of the weight of a given volume of fluid to the weight of an equal volume of water at 4°C is called: Viscosity Specific weight Specific gravity Density Specific gravity compares the density of a fluid to that of water, making it dimensionless. 100 / 100 Which of the following properties defines the resistance of a fluid to shear deformation? Density Viscosity Compressibility Specific weight Viscosity measures a fluid’s internal resistance to motion or flow — higher viscosity means thicker flow. Your score isThe average score is 34% 0% Restart quiz