2.2.1 · D3 · Physics › Fluid Mechanics › Fluid definition — shear stress, no fixed shape
Yeh practice deep-dive hai parent note ke liye. Wahan humne law τ = μ d y d u banaya tha. Yahan hum ise har us situation ke against maarte hain jo topic throw kar sakta hai — including weird wale (zero gap, non-linear profile, "yeh solid hai" wale traps). Pehle matrix padho, phir har example karo apna answer forecast karne ke baad .
Recall Symbols jo hum use karenge (sab parent note mein earn kiye hain)
τ ::: shear stress = tangential force per area, units Pa.
μ ::: dynamic viscosity, units Pa·s (fluid ki "thickness").
d u / d y ::: velocity gradient = layer ki speed kitni tezi se badal rahi hai jaise upar jaate hain, units s − 1 .
F t ::: tangential (shear) force, units N.
A ::: contact area, units m 2 .
γ , γ ˙ ::: shear strain (ek angle), aur uska rate of change d u / d y .
Fluid definition + Newton's viscosity law ke baare mein sab kuch in case-classes tak reduce hota hai. Neeche har worked example us cell ke saath tagged hai jo woh fill karta hai.
Cell
Case class
Kya tricky hai
Example
A
Linear profile, seedha plug-in
kuch nahi — yeh baseline hai
Ex 1
B
τ se force / area recover karna
A se multiply karo wapas
Ex 2
C
Unknown μ solve karna
law ko rearrange karo
Ex 3
D
Static fluid, γ ˙ = 0
answer hai zero — degenerate case
Ex 4
E
Non-linear velocity profile
local slope (derivative) use karna padega
Ex 5
F
Limiting behaviour: gap → 0
gradient blow up hota hai
Ex 6
G
Real-world word problem
words ko u , y , A , μ mein translate karo
Ex 7
H
Exam twist: solid-vs-fluid decision
kya yeh G γ hai ya μ γ ˙ ?
Ex 8
I
Unit / sanity trap (mm vs m)
divide karne se pehle convert karo
Ex 9
Worked example Seedha plug-in
Water film, viscosity μ = 1.0 × 1 0 − 3 Pa·s, gap y = 5 mm , top plate speed u = 0.4 m/s, linear profile. τ find karo.
Forecast: water patla hai, toh expect karo chhota number of pascals.
Step 1 — Gap convert karo: y = 5 mm = 0.005 m.
Yeh step kyun? Formula ke units SI hain; mm dene se 1000× error aayega.
Step 2 — Linear profile ⇒ gradient bas (speed)/(gap) hai:
d y d u = 0.005 0.4 = 80 s − 1 .
Yeh step kyun? Straight-line profile ka slope constant hota hai, toh d u / d y = rise/run.
Step 3 — Newton's law apply karo:
τ = μ d y d u = ( 1.0 × 1 0 − 3 ) ( 80 ) = 0.08 Pa .
Yeh step kyun? Yeh Newtonian fluid ke liye shear stress ki definition hi hai.
Verify: units Pa⋅s × s − 1 = Pa ✓. Aur 0.08 Pa bahut chhota hai — "water patla hai" se match karta hai. ✓
Worked example Stress se wapas force tak
Ex 1 mein plate ka area A = 0.25 m 2 hai. Ise steadily move rakhne ke liye kitna sideways force chahiye?
Forecast: stress tiny tha, area 1 m 2 se kam hai, toh force ek newton ka fraction hoga.
Step 1 — Ex 1 se τ = 0.08 Pa use karo.
Yeh step kyun? Same film, same conditions — stress unchanged hai.
Step 2 — Stress force per area hai, toh invert karo: F t = τ A .
F t = 0.08 × 0.25 = 0.02 N .
Yeh step kyun? τ = F t / A ⇒ F t = τ A ; area se multiply karna "per area" ko undo karta hai.
Verify: units Pa × m 2 = ( N/m 2 ) × m 2 = N ✓. Steady speed ⇒ yeh force exactly viscous drag ko balance karta hai (Newton's 1st law). ✓
μ
Ek unknown oil ke upar A = 0.5 m 2 area ki plate drag karte hain, gap 2 mm , plate speed 0.3 m/s, aur measured force F t = 7.5 N lagti hai. μ find karo.
Forecast: oils water se "thicker" hote hain, toh expect karo μ tenths of Pa·s ke around, 1 0 − 3 nahi.
Step 1 — Measured force se stress nikalo: τ = F t / A = 7.5/0.5 = 15 Pa.
Yeh step kyun? Hum force measure karte hain, lekin law stress mein likha hai — pehle convert karo.
Step 2 — Gradient: d u / d y = 0.3/0.002 = 150 s − 1 .
Yeh step kyun? Linear profile, phir se rise/run.
Step 3 — μ ke liye law rearrange karo:
μ = d u / d y τ = 150 15 = 0.1 Pa⋅s .
Yeh step kyun? τ = μ ( d u / d y ) , toh μ isolate karne ke liye stress ko gradient se divide karo.
Verify: 0.1 Pa·s water se 100× zyada hai — "oil" se consistent. Plug back karo: 0.1 × 150 = 15 Pa ✓.
Worked example Zero rate of strain
Paani ka ek glass table par bilkul still rakha hai. Uske andar shear stress kya hai?
Forecast: fluid ki defining property yahan dikhni chahiye — aage padhne se pehle guess karo.
Step 1 — Kuch move nahi kar raha, toh har layer ki speed same (zero) hai: u ( y ) = 0 har jagah.
Yeh step kyun? "At rest" ka matlab hai velocity field identically zero hai.
Step 2 — Isliye gradient hai d u / d y = 0 .
Yeh step kyun? Ek constant ka (yahan, zero) slope zero hota hai.
Step 3 — Law apply karo: τ = μ × 0 = 0 .
τ = 0 Pa .
Yeh step kyun? Rate of strain nahi ⇒ viscous stress nahi.
Verify: Yeh bilkul fluid ki definition hai — yeh static equilibrium par zero shear sustain karta hai . Agar τ nonzero hota toh paani abhi bhi flow kar raha hota, jo "at rest" ka contradict karta. ✓ (Dekho Hydrostatics — Fluids at Rest — sirf normal pressure bachti hai.)
Worked example Curved velocity profile
Fluid ek wall ke paas measured profile u ( y ) = 50 y − 2500 y 2 ke saath flow karta hai (SI units, valid hai 0 ≤ y ≤ 0.01 m ke liye). Viscosity μ = 0.02 Pa·s. Shear stress find karo bilkul wall par (y = 0 ) aur y = 4 mm par.
Forecast: profile wall par sabse steep hai, toh shear sabse zyada y = 0 par hona chahiye aur upar jaane par chhhota.
Step 1 — Curved profile ke liye hum "speed/gap" use nahi kar sakte. Hume local slope chahiye, yaani derivative — yahi d y d u ka matlab hai.
Yeh tool kyun, rise/run nahi? Rise/run sirf straight lines ke liye kaam karta hai. Derivative har point par tangent ka slope deta hai — wahan ka honest velocity gradient. Figure mein do tangent lines dekho: unki steepness alag hai.
d y d u = 50 − 5000 y .
Step 2 — Wall par, y = 0 : d u / d y = 50 s − 1 , toh
τ wall = 0.02 × 50 = 1.0 Pa .
Yeh step kyun? Wall stress y = 0 par evaluate kiya hua slope use karta hai.
Step 3 — y = 4 mm = 0.004 m par: d u / d y = 50 − 5000 ( 0.004 ) = 50 − 20 = 30 s − 1 , toh
τ = 0.02 × 30 = 0.6 Pa .
Yeh step kyun? Same derivative, naye height par evaluate kiya.
Verify: 1.0 > 0.6 ✓ — wall se door jaane par shear girta hai, forecast se match karta hai (profile flat hota jaata hai). Units Pa⋅s × s − 1 = Pa ✓.
Common mistake Curved profile par
u / y use karna
Yeh sahi kyun lagta hai: Ex 1 mein kaam kiya tha. Fix: u / y 0 se y tak ka average slope hai; physics ko local slope d u / d y chahiye. Sirf straight-line profiles ke liye yeh dono equal hote hain.
y → 0 hota hai toh kya hota hai?
Plate speed u = 0.3 m/s aur viscosity μ = 0.1 Pa·s fixed rakho. Gaps y = 2 mm, 0.5 mm, 0.1 mm ke liye τ compute karo. Trend kya hai?
Forecast: same speed par thinner film squeeze karna = shear karna mushkil. Guess: τ badhega.
Step 1 — Har gap par gradient: d u / d y = u / y .
y = 0.002 : 150 s − 1
y = 0.0005 : 600 s − 1
y = 0.0001 : 3000 s − 1
Yeh step kyun? Same speed chhote gap par → steeper gradient.
Step 2 — μ = 0.1 se multiply karo:
τ = 15 Pa , 60 Pa , 300 Pa .
Yeh step kyun? Naye gradients ke saath Newton's law.
Step 3 — Limit lo: jab y → 0 , y u → ∞ , toh τ → ∞ .
Yeh step kyun? Fixed speed ko shrinking gap se divide karna bina bound ke badhta hai.
Verify: gap ko half karne par τ double hota hai (15 → ... y 4 se cut ⇒ τ × 4 = 60 ✓; 20 se cut ⇒ × 20 = 300 ✓). Physically: isliye thin lubricant films enormous shear resist karte hain — bearings ki yahi basis hai.
Worked example Skater paani ki film par
Ek ice skater ka blade (A = 6.0 cm 2 ) 10 μ m melt-water film (μ = 1.8 × 1 0 − 3 Pa·s) par 8 m/s ki speed se glide karta hai. Skater ko resist karne wala viscous drag force kya hai?
Forecast: super-thin film + real speed → sizeable gradient, lekin water patla hai aur area tiny hai; expect karo ek newton ka fraction.
Step 1 — Words ko symbols mein translate karo: A = 6.0 cm 2 = 6.0 × 1 0 − 4 m 2 , y = 10 μ m = 1.0 × 1 0 − 5 m, u = 8 m/s.
Yeh step kyun? Formula ko touch karne se pehle har quantity SI honi chahiye.
Step 2 — Gradient (linear film): d u / d y = 8/ ( 1.0 × 1 0 − 5 ) = 8.0 × 1 0 5 s − 1 .
Yeh step kyun? Thin film, toh large gradient — drag wahan se aata hai.
Step 3 — Stress: τ = μ ( d u / d y ) = ( 1.8 × 1 0 − 3 ) ( 8.0 × 1 0 5 ) = 1440 Pa.
Yeh step kyun? Newton's law.
Step 4 — Force: F t = τ A = 1440 × 6.0 × 1 0 − 4 = 0.864 N.
Yeh step kyun? Blade area ke zariye stress ko wapas force mein convert karo.
Verify: ek fast skater par ≈ 0.86 N ka drag believable hai (ice famously low-friction hai). Units check: Pa·s × s⁻¹ × m² = N ✓.
Worked example Kaun sa law apply hota hai?
Rubber ka ek block (G = 5 × 1 0 5 Pa) steady shear τ = 2 × 1 0 4 Pa se push kiya jaata hai. (a) Uska steady shear strain γ find karo. (b) Ek dost insist karta hai ki rubber "flows" aur τ = μ γ ˙ use karta hai. Kaun sahi hai?
Forecast: rubber tilt hoke ruk jaata hai — yeh solid behaviour hai, toh iska finite γ hoga.
Step 1 — Material class decide karo. Rubber fixed deformation tak pahunchta hai aur use hold karta hai, toh yeh ek solid hai → τ = G γ use karo, viscosity law nahi .
Yeh step kyun? Pura topic is fork par depend karta hai: solids shear store karte hain (G γ ), fluids nahi kar sakte (μ γ ˙ ). Law galat choose karna classic trap hai.
Step 2 — Strain solve karo: γ = τ / G = ( 2 × 1 0 4 ) / ( 5 × 1 0 5 ) = 0.04 (ek pure number = tilt ke radians).
γ = 0.04.
Yeh step kyun? τ = G γ ⇒ γ = τ / G .
Step 3 — Dost ko judge karo: ek fluid hamesha tilt karta rahta (γ ˙ > 0 forever). Rubber nahi karta — woh settle ho jaata hai. Toh dost galat hai; fluid law apply nahi hota.
Yeh step kyun? Defining test hai "kya yeh deform karna jaari rakhta hai?" Rubber kehta hai nahi.
Verify: γ = 0.04 rad ≈ 2.3° tilt — chhota aur steady, bilkul waisa jaise ek solid behave kare. Stress and Strain in Solids se contrast karo. ✓
Worked example mm-vs-m error dhundho
Ek student glycerin (μ = 1.4 Pa·s) mein shear compute karta hai, plate speed 0.6 m/s, gap 3 mm, aur likhta hai d u / d y = 0.6/3 = 0.2 s − 1 , toh τ = 0.28 Pa. Error dhundho aur sahi τ batao.
Forecast: glycerin bahut thick hai; 0.28 Pa suspiciously tiny lagta hai. Kuch gadbad hai.
Step 1 — Diagnose karo: student ne 3 mm ko 3 express karke divide kiya, metres mein convert karna bhool gaya.
Yeh step kyun? d u / d y hona chahiye (m/s)/(m); m/s ko mm ke saath mix karna silently answer mein 1000 ka error daal deta hai.
Step 2 — Correct gap: y = 3 mm = 0.003 m, toh d u / d y = 0.6/0.003 = 200 s − 1 .
Yeh step kyun? Consistent SI units.
Step 3 — Correct stress: τ = 1.4 × 200 = 280 Pa.
τ = 280 Pa .
Yeh step kyun? Fixed gradient ke saath Newton's law.
Verify: sahi answer exactly galat answer ka 1000 × hai (0.28 → 280 ) — yeh mm/m slip ki signature hai. Aur thick glycerin ke liye 280 Pa reasonable hai, unlike 0.28 Pa. ✓
Recall Quick self-test (right side cover karo)
Linear profile, gradient ke liye kaun sa formula? ::: d u / d y = u / y .
Curved profile, gradient ke liye kaun sa tool? ::: derivative d u / d y locally evaluate kiya hua.
Fluid at rest, shear stress? ::: bilkul zero (defining property).
Fixed speed par gap y → 0 hone par, τ kya karta hai? ::: bina bound ke badhta hai (→ ∞ ).
Rubber steady shear ke under — kaun sa law? ::: τ = G γ (yeh solid hai, finite strain).
Numbers plug karne se pehle sabse pehle kya check karo? ::: mm/cm/µm ko metres mein convert karo.
Mnemonic Case-check ritual
"CLUES" — C lass (solid ya fluid?), L inear ya curved (rise/run vs derivative?), U nits (sab SI?), E valuate the gradient, S cale-check the answer.
Velocity Profile and No-Slip Condition — jahan Ex 5 jaisi curved profiles aati hain.
Viscosity and Newtonian vs Non-Newtonian Fluids — throughout use kiye gaye μ par deeper dive.
Hydrostatics — Fluids at Rest — Ex 4 ki γ ˙ = 0 duniya.
Stress and Strain in Solids — Ex 8 ka τ = G γ side.
Pressure in Fluids — shear ka normal-stress companion.