Derivation (from scratch). Take a streamline at the same height h, from a point far upstream (1) with speed v and static pressure P0, to the stagnation mouth (2) where v2=0 and pressure Ps:
P0+21ρv2=Ps+0Why this step? Heights are equal, so ρgh cancels; point 2 is at rest by definition of stagnation.
Derivation. Horizontal pipe (h1=h2), wide section (1) and throat (2):
P1+21ρv12=P2+21ρv22⇒P1−P2=21ρ(v22−v12)
Continuity gives v1=A1A2v2. Substitute:
P1−P2=21ρv22(1−A12A22)Why this step? We replaced v1 to leave a single unknown v2. Solve for v2 and multiply by A2 to get Q:
Derivation. Surface (1) at the top, hole (2) at depth H. Both open to atmosphere so P1=P2=Patm. If hole area ≪ tank area, v1≈0:
Patm+0+ρgH=Patm+21ρv2+0Why this step? Pressures cancel; surface speed ≈0 by continuity (Ahole≪Atank); set hole as height reference.
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.
Dekho, teeno devices ka dil ek hi hai: Bernoulli + Continuity. Bernoulli kehta hai ki ek streamline pe P+21ρv2+ρgh 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=0), aur uski speed wali energy extra pressure ban jaati hai. Static pressure se difference lo, aur v=2ΔP/ρ se speed nikal lo — yahi se plane apni airspeed maapta hai.
Venturi meter: pipe ko beech mein patla kar do. Continuity (A1v1=A2v2) 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(A12−A22)] nikal lo. Yaad rakhna: patla matlab tez aur kam pressure, na ki zyada pressure — yahan log galti karte hain.
Orifice (Torricelli): tank mein depth H 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=2gH — bilkul jaise koi cheez H height se gir rahi ho. Jet ki horizontal range x=2Hy projectile motion se aati hai. Mantra: Push, Pinch, Pour — Pitot, Venturi, Orifice. Exam mein yeh teen formula aur unki derivation guaranteed marks hai.