2.2.16Fluid Mechanics

Applications — Pitot tube, Venturi meter, orifice flow

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Three classic devices that turn Bernoulli's equation into a measuring tool. Master one idea — trade pressure for speed — and all three fall out.


0. The tools we derive everything from

We will only combine these two. Nothing else is needed.


1. Pitot tube — measuring the speed of a flow

Derivation (from scratch). Take a streamline at the same height hh, from a point far upstream (1) with speed vv and static pressure P0P_0, to the stagnation mouth (2) where v2=0v_2=0 and pressure PsP_s: P0+12ρv2=Ps+0P_0 + \tfrac12\rho v^2 = P_s + 0 Why this step? Heights are equal, so ρgh\rho g h cancels; point 2 is at rest by definition of stagnation.

So the dynamic pressure is PsP0=12ρv2P_s - P_0 = \tfrac12\rho v^2. Solve:


2. Venturi meter — measuring flow rate in a pipe

Derivation. Horizontal pipe (h1=h2h_1=h_2), wide section (1) and throat (2): P1+12ρv12=P2+12ρv22    P1P2=12ρ(v22v12)P_1+\tfrac12\rho v_1^2 = P_2+\tfrac12\rho v_2^2 \;\Rightarrow\; P_1-P_2=\tfrac12\rho(v_2^2-v_1^2) Continuity gives v1=A2A1v2v_1 = \dfrac{A_2}{A_1}v_2. Substitute: P1P2=12ρv22(1A22A12)P_1-P_2=\tfrac12\rho\,v_2^2\left(1-\frac{A_2^2}{A_1^2}\right) Why this step? We replaced v1v_1 to leave a single unknown v2v_2. Solve for v2v_2 and multiply by A2A_2 to get QQ:

Figure — Applications — Pitot tube, Venturi meter, orifice flow

3. Orifice flow (Torricelli) — fluid draining from a tank

Derivation. Surface (1) at the top, hole (2) at depth HH. Both open to atmosphere so P1=P2=PatmP_1=P_2=P_{atm}. If hole area \ll tank area, v10v_1\approx 0: Patm+0+ρgH=Patm+12ρv2+0\cancel{P_{atm}}+0+\rho g H = \cancel{P_{atm}}+\tfrac12\rho v^2+0 Why this step? Pressures cancel; surface speed 0\approx0 by continuity (AholeAtankA_{hole}\ll A_{tank}); set hole as height reference.


Forecast-then-Verify

Recall Predict before you compute
  1. If you double the venturi pressure drop, does QQ double? NoQΔPQ\propto\sqrt{\Delta P}, so it rises by 21.41×\sqrt2\approx1.41\times.
  2. Two holes, one at depth HH and one at 4H4H. Speed ratio? 1:21:2 (since vHv\propto\sqrt H).
  3. Pitot in water vs air for same ΔP\Delta P — which gives larger vv? Air, because v1/ρv\propto1/\sqrt\rho and air is lighter.

Common mistakes (steel-manned)


80/20 — the highest-yield takeaways

  • Every device = Bernoulli + Continuity, then solve for a speed.
  • Pitot: v=2ΔP/ρv=\sqrt{2\Delta P/\rho}. Venturi: Q=A1A22ΔPρ(A12A22)Q=A_1A_2\sqrt{\tfrac{2\Delta P}{\rho(A_1^2-A_2^2)}}. Orifice: v=2gHv=\sqrt{2gH}.
  • Faster fluid ⇒ lower pressure. Memorize that arrow and you can re-derive all three.

Recall Feynman: explain to a 12-year-old

Imagine running in a hallway. In a narrow part you have to speed up to get through (that's continuity). When you rush, you push less on the side walls (low pressure) — when you stand still you lean on the wall more (high pressure). A pitot tube is like sticking your hand straight into the wind: you feel a hard push that tells you how fast the wind is. A venturi is the narrow hallway: the squeeze makes water race and press lightly, and we read that. An orifice is a hole in a water bucket: the deeper the hole, the more "fall" the water gets, so it squirts out faster — exactly like dropping a stone from that depth.


Connections

  • Bernoulli's Equation — the parent principle.
  • Continuity Equation — supplies the A1v1=A2v2A_1v_1=A_2v_2 link.
  • Torricelli's Law — special case of orifice flow.
  • Projectile Motion — used for the orifice jet range.
  • Manometers and Pressure Measurement — how ΔP\Delta P is read as Δh\Delta h.
  • Dynamic vs Static vs Stagnation Pressure.

Flashcards

What is a stagnation point?
A point where the fluid is brought to rest (v=0v=0), converting kinetic energy into extra (stagnation) pressure.
Pitot tube speed formula
v=2(PsP0)/ρv=\sqrt{2(P_s-P_0)/\rho}, where PsP0P_s-P_0 is the dynamic pressure.
Why is throat pressure lower in a venturi?
Continuity forces higher speed at the smaller throat; Bernoulli then requires lower pressure for constant total energy.
Venturi volume flow rate
Q=A1A22(P1P2)ρ(A12A22)Q=A_1A_2\sqrt{\dfrac{2(P_1-P_2)}{\rho(A_1^2-A_2^2)}}.
State Torricelli's law
Efflux speed from a hole at depth HH is v=2gHv=\sqrt{2gH}, same as free fall through HH.
Does orifice speed depend on hole area?
No — speed is 2gH\sqrt{2gH}; area only changes the flow rate Q=A2gHQ=A\sqrt{2gH}.
Horizontal range of an orifice jet (hole depth H, height y above floor)
x=2Hyx=2\sqrt{Hy}.
If venturi ΔP\Delta P doubles, how does QQ change?
Increases by 21.41×\sqrt2\approx1.41\times, since QΔPQ\propto\sqrt{\Delta P}.
Two equations that derive all three devices
Bernoulli (P+12ρv2+ρgh=P+\tfrac12\rho v^2+\rho gh=const) and Continuity (A1v1=A2v2A_1v_1=A_2v_2).
Converting ΔP\Delta P to manometer height
ΔP=(ρmρ)gΔh\Delta P=(\rho_m-\rho)g\,\Delta h for a fluid column of density ρm\rho_m.

Concept Map

implies

combined with

exploited by

solves for unknown speed

solves for unknown speed

applied to

uses

gives dynamic pressure

yields

throat speeds up

yields

yields

Bernoulli equation

Continuity A1 v1 = A2 v2

Faster flow = lower pressure

Measure pressure difference

Pitot tube

Venturi meter

Orifice flow

Speed of flow

Flow rate Q

Drain speed

Stagnation point v=0

Hinglish (regional understanding)

Intuition Hinglish mein samjho

Dekho, teeno devices ka dil ek hi hai: Bernoulli + Continuity. Bernoulli kehta hai ki ek streamline pe P+12ρv2+ρghP+\tfrac12\rho v^2+\rho gh constant rehta hai — yani jahan fluid tez bhaagta hai, wahan pressure kam ho jaata hai. Bas yahi ek line yaad rakho, baaki sab isi se nikal aata hai.

Pitot tube: ek tube ko seedha flow ke saamne rakho. Wahan fluid ruk jaata hai (stagnation point, v=0v=0), aur uski speed wali energy extra pressure ban jaati hai. Static pressure se difference lo, aur v=2ΔP/ρv=\sqrt{2\Delta P/\rho} se speed nikal lo — yahi se plane apni airspeed maapta hai.

Venturi meter: pipe ko beech mein patla kar do. Continuity (A1v1=A2v2A_1v_1=A_2v_2) ki wajah se throat mein fluid tez ho jaata hai, aur Bernoulli ke hisaab se wahan pressure gir jaata hai. Us pressure drop ko manometer se padho aur flow rate Q=A1A22ΔP/[ρ(A12A22)]Q=A_1A_2\sqrt{2\Delta P/[\rho(A_1^2-A_2^2)]} nikal lo. Yaad rakhna: patla matlab tez aur kam pressure, na ki zyada pressure — yahan log galti karte hain.

Orifice (Torricelli): tank mein depth HH pe chhota chhed karo. Upar aur chhed dono jagah atmospheric pressure, to sirf gravity ki height bachti hai jo speed mein badal jaati hai: v=2gHv=\sqrt{2gH} — bilkul jaise koi cheez HH height se gir rahi ho. Jet ki horizontal range x=2Hyx=2\sqrt{Hy} projectile motion se aati hai. Mantra: Push, Pinch, Pour — Pitot, Venturi, Orifice. Exam mein yeh teen formula aur unki derivation guaranteed marks hai.

Go deeper — visual, from zero

Test yourself — Fluid Mechanics

Connections