Intuition The one core idea
A moving fluid carries its energy in three forms — pressure, motion, and height — and the total never changes along a streamline. Every device in this topic just swaps one form for another (motion for pressure, or height for motion) and reads the swap with a tube.
Before you can trust the Pitot / Venturi / Orifice formulas, you must be able to read them. Below is every symbol and idea the parent note leans on, built from nothing, each one earning the next.
Definition Fluid particle
A fluid particle is an imaginary tiny blob of the liquid or gas, small enough that it moves as one piece but big enough to have a definite pressure and speed.
A streamline is the path one fluid particle traces as it flows — like the line a single leaf follows down a river. We always apply energy bookkeeping along one streamline , following the same blob from point 1 to point 2.
Why the topic needs it: every derivation says "point 1 ... point 2 ... along a streamline." That phrase means: pick one blob and watch it travel from the wide pipe to the throat, or from the tank surface to the hole. Without the streamline picture, the equation is just symbols.
ρ (Greek "rho")
ρ = mass packed into each cubic metre of the fluid, in kg/m 3 .
ρ = volume mass
Picture a 1 m × 1 m × 1 m box of the fluid: ρ is how many kilograms that box weighs. Water ≈ 1000 , air ≈ 1.2 .
Why the topic needs it: energy in a fluid is bookkept per unit volume , and to turn "how fast" into "how much energy" you must know how much mass sits in each volume — that is exactly ρ . It is why a Pitot tube gives a different speed in air vs water for the same push.
P
P = force pushing outward on each square metre of surface, in pascals (Pa = N/m 2 ).
P = area force
Intuition Pressure has no direction of its own
A fluid at a point pushes equally in every direction . Look at the red arrows in the figure — they fan out all around the point. That is why a side-hole (static port) and a face-on hole (stagnation port) can read different pressures: it is not the direction of pressure that changes, it is whether the flow is allowed to slam to a stop.
Why the topic needs it: all three devices measure a pressure difference P 1 − P 2 and convert it to a speed. Pressure is the quantity the tubes actually sense.
v and cross-sectional area A
v = how fast a fluid particle moves (m/s ).
A = the area of the "window" the fluid flows through, measured straight across the pipe (m 2 ).
Picture slicing the pipe with a knife perpendicular to the flow — the face you expose is A .
Common mistake Reading areas in cm² and forgetting to convert
1 cm 2 = 1 0 − 4 m 2 , so 10 cm 2 = 1 0 − 3 m 2 . Mixing cm 2 into an SI formula silently ruins the answer. Fix: convert every length/area to metres before substituting.
Definition Volume flow rate
Q
Q = volume of fluid crossing a section each second, in m 3 / s .
Q = A v
Why A v ? In one second a particle moving at v travels a distance v , so it sweeps out a cylinder of length v and face A — volume A v .
Why the topic needs it: Continuity Equation gives the second equation (besides Bernoulli) that lets us eliminate one unknown speed and solve for the other.
h and gravity g
h = how high the point sits above some chosen reference level (m ).
g ≈ 9.8 m/s 2 (often 10 in exams) = strength of gravity's pull.
ρ g h is an "energy per volume"
Lifting a volume of fluid of mass ρ V up by height h takes work ρ V g h . Divide by the volume V and you get ρ g h — the stored energy per unit volume just for being high up. In the orifice tank, this stored height-energy is what becomes the jet's speed.
Why the topic needs it: the ρ g h term drives Torricelli's draining tank. In a horizontal Pitot or Venturi, h 1 = h 2 so this term simply cancels.
2 1 ρ v 2 is called the dynamic pressure — the "cost" of moving.
P (the ordinary sensed push) is the static pressure .
P + 2 1 ρ v 2 (what a face-on tube reads when it stops the flow) is the stagnation pressure .
See Dynamic vs Static vs Stagnation Pressure for these three names, and Bernoulli's Equation for the full derivation.
2 1 ρ v 2 and not ρ v or ρ v 2 ?
Kinetic energy of a mass m is 2 1 m v 2 . Per unit volume, mass m becomes ρ , giving 2 1 ρ v 2 . The square is why doubling a pressure drop only multiplies speed by 2 — a recurring theme in this topic.
Definition Manometer height
Δ h
A manometer is a U-tube of liquid (density ρ m ) connected between two ports. The pressure difference pushes the liquid up by a height Δ h , and
P 1 − P 2 = ρ m g Δ h .
So a pressure difference you cannot see becomes a height you can read with a ruler.
Why the topic needs it: real Pitot and Venturi meters don't display Pa — they display a fluid column Δ h . See Manometers and Pressure Measurement .
Fluid particle on a streamline
Kinetic term half rho v squared
Bernoulli P + half rho v squared + rho g h
Read it top-down: the raw ideas (particle, density, height) feed the two master tools (Bernoulli, Continuity), which together power all three devices.
Test yourself — cover the right side and answer before revealing.
What does a streamline represent physically? The path a single fluid particle follows as it flows.
Units and meaning of density ρ ? Mass per unit volume, kg/m 3 .
Why does pressure push equally in all directions? In a fluid at a point there is no preferred direction; force per area is the same every way.
Convert 5 cm 2 to SI. 5 × 1 0 − 4 m 2 .
State continuity in words. The same volume per second crosses every cross-section, so narrow means fast.
Why does the kinetic term carry a factor 2 1 ? Kinetic energy is 2 1 m v 2 ; per volume, m → ρ , giving 2 1 ρ v 2 .
What are the units of every term in Bernoulli? Pascals — energy per unit volume.
How does a manometer turn a pressure difference into something readable? P 1 − P 2 = ρ m g Δ h — the difference lifts a liquid column of height Δ h .
If Δ P doubles, how does speed change? It grows by
2 ≈ 1.41 , since
v ∝ Δ P .