(a) Lspin axis ke saath point karta hai (upar aur tilt hua; sense spin ke around right-hand rule se set hota hai).
(b) τ=r×mghorizontal hai, us vertical plane ke perpendicular jisme axis hai. Gravity seedha neeche hai, r axis ke upar hai, toh unka cross product horizontal hai — yeh kabhi neeche point nahi kar sakta.
(c) dL=τdtτ ke same direction mein point karta hai — horizontal. Isliye axis sideways swing karta hai (precess karta hai) girne ki bajaye.
Neeche in teeno vectors ki picture dekho.
Recall Solution
Upar (faster precession): arm length r, mass m, gravity g — yeh sab milke torque rmg hain.
Neeche (slower precession): moment of inertia I aur spin rate ω — yeh sab milke spin angular momentum L=Iω hain.
Tilt θ: yeh cancel ho gaya. Yeh ek baar τ=rmgsinθ mein appear karta hai (numerator) aur ek baar horizontal projection Lsinθ mein (denominator), toh Ω fast-spin limit mein tilt se independent hai.
Ω=rmg/(Iω), toh Ω∝1/ω. ω ko triple karne se Ωek-tihai reh jaata hai.
Period rate ka inverse hai: T=2π/Ω, toh T∝ω. ω ko triple karne se period triple ho jaata hai.
T2=3×6.0=18.0s.
Recall Solution
Kisi bhi θ par: τ=rmgsinθ=0.50sinθ, aur horizontal projection Lsinθ=2.0sinθ hai.
θ=30°: Ω=2.0sin30°0.50sin30°=2.00.50=0.25rad/s.
θ=75°: Ω=2.0sin75°0.50sin75°=2.00.50=0.25rad/s.
sinθ upar aur neeche dono se divide ho jaata hai — dono tilts ke liye same Ω=0.25rad/s. Neeche ka figure dikhata hai kyun: L ki tip ke trace kiye horizontal circle ka radius Lsinθ hai, jo bilkul match karta hai ki torque kaise badhta hai.
r=rx^ likho (iska horizontal lean; vertical part g ke parallel hai aur cross product mein kuch contribute nahi karta), aur mg=−mgz^.
(a) τ=(rx^)×(−mgz^)=−rmg(x^×z^). Ab x^×z^=−y^, toh τ=−rmg(−y^)=+rmgy^. τ+y direction mein point karta hai.
(b) dL=τdt+y ke saath hai, toh axis (jo +x ki taraf jhuki thi) +y ki taraf swing karegi.
(c) +x→+y→−x→−y jaana upar se dekha jaaye toh counter-clockwise hai (+z axis ke upar se neeche dekhte hue). Figure dekho.
(a) τ=rmg=0.03×0.20×9.8=0.0588N⋅m. L=Iω=0.004×8.0=0.032kg⋅m2/s. Ω=τ/L=0.0588/0.032=1.8375rad/s.
(b) Ratio Ω/ω=1.8375/8.0=0.2297, yaani lagbhag 23%. Yeh ≪1nahi hai. Fast-spin approximation shaky hai: jo physics neglect ho rahi hai woh nutation hai — axis precess karte waqt clearly upar-neeche bob karega, aur sach mein averaged Ω is value se thoda alag hoga. Clean steady precession ke liye ω ko das ya zyada times bada chahiye hoga.
Recall Solution
(a) Jaise ω→0, denominator Iω→0, toh Ω→∞. Formula infinitely fast precession predict karta hai.
(b) Physically ek non-spinning top simply gir jaata hai — koi precession nahi. Yeh contradiction formula ka apna breakdown dikhana hai: ω=0 ke saath koi angular momentum redirect karne ke liye nahi hai, toh τ=dL/dt simply L ko torque ki direction mein zero se build up karta hai — top topple kar jaata hai. Formula Ω=rmg/(Iω) sirf fast-spin limit mein valid hai jahan pehle se ek bada L exist karta hai jo steer kiya ja sake; "Ω→∞" iska tarika hai yeh kehne ka ki "main yahan apply nahi hota."
Recall Solution
(a) ΩA=τ/LA=2.0/4.0=0.50rad/s. ΩB=τ/LB=2.0/12.0=0.16=0.1667rad/s.
(b) ΩA/ΩB=0.50/0.1667=3.0. Gyro B precesses 3× slower — bilkul ratio LB/LA=3 jaisa. Bada L ⇒ same torque par slower response.
(c) Ek bullet jise bada spin L diya gaya ho, uska kisi bhi cross-wind ya gravity torque ke liye tiny Ω hoga, toh flight ke dauran uski naak barely axis se bhatakti hai — yahi spin-stabilisation hai, wahi principle jo Gyroscope and Navigation system mein use hoti hai.