Laboratory 3 Forces Michael Akopov PH1004 Section E2 Abstract The objective of this lab was to explore and analyze general collisions between two items. A In this experiment, an air track was used to investigate the conservation of momentum and kinetic energy for elastic collisions, and the conservation of momentum for inelastic collisions. A collision is an isolated event in which each colliding particle exerts a force on the other particle for a relatively short period of time. Collisions happen every time one object comes into contact with another and physical energy is altered. Collisions can be grouped into elastic collisions, inelastic collisions, and perfectly inelastic collisions. Elastic collisions are such collisions that the kinetic energy and the momentum of the system are conserved. Inelastic collisions are such collisions where only momentum is conserved. A perfectly inelastic collisions is one after which the objects stick together and move with one velocity as one unit. The two types of collisions observed in this experiment were elastic and perfectly inelastic collisions. In the first part we had to see if the collisions that happened were really elastic. For the elastic collision we used mathematics to prove that the kinetic energy and momentum were conserved. For the perfectly inelastic collision we had to show that there was no conservation in the kinetic energy but only momentum conservation. For part A and part B, the results proved the above implication, and the experiment was thereby successful. Data Variables Symbol xb1 xub1 xb2 xub2 x Description Position of blocked photogate for flag 1 Position of unblocked photogate for flag 1 Position of blocked photogate for flag 2 Position of unblocked photogate for flag 2 Distance measurement uncertainty Measurement tool Ruler Ruler Ruler Ruler Ruler m1 m2 m1 m2 Glider1 Mass Glider 2 Mass Glider 1 Mass measurement uncertainty Glider 2 Mass measurement uncertainty tb1i tb1f tb2f Initial time when Glider 1 passes photogate 1 Final time when Glider 1 passes photogate 2 Final time when Glider 2 passes photogate 3 Final time when Glider 1 + 2 pass photogate 2 (B) Time measurement uncertainty tb(1&2)f t xf1 xf2 xf1 xf2 Digital Scale Digital Scale Digital Scale Digital Scale Computer Clock Computer Clock Computer Clock Computer Clock Given (0.001s) Flag 1 width Flag 2 width Flag 1 Width measurement uncertainty Flag 2 Width measurement uncertainty Ruler Ruler Ruler Ruler Part A Table 1: Data from part a of the experiment Trial tb1i 1 0.068 s 2 0.068 s 3 0.070 s 4 0.068 s 5 0.069 s 6 0.071 s 7 0.069 s 8 0.069 s 9 0.070s 10 0.069s tb1f 0.244 s 0.228 s 0.240 s 0.230 s 0.235 s 0.224 s 0.220 s 0.191 s 0.247 s 0.221 s tb2f 0.057 s 0.057 s 0.057 s 0.056 s 0.056 s 0.058 s 0.057 s 0.059 s 0.058 s 0.057 s xb1 xub1 xb2 xub2 x m1 m2 m t 50.0 cm 52.5 cm 50.0 cm 52.5 cm 0.05 cm 406 g 205 g 0.05 g 0.001 s Table 2: flag measurement and instrumental uncertainty xb1 50.0 cm xub2 52.5 cm xf1 2.5cm xf1 0.05 cm xb2 50.0 cm xub2 52.5 cm xf2 2.5cm Part B Table 3: Data from part b of the experiment Trial 1 2 3 4 5 6 7 8 9 10 tb1i 0.069 s 0.069 s 0.070 s 0.069 s 0.069 s 0.070 s 0.070 s 0.069 s 0.069 s 0.069 s tb(1&2)f 0.117 s 0.114 s 0.111 s 0.111 s 0.111 s 0.113 s 0.112 s 0.113 s 0.116 s 0.119 s m1 m2 m1 m2 t 406 g 205 g 0.05 g 0.05 g 0.001 s xf2 0.05 cm Analysis Part A: 1. The width of the flags was determined by subtracting the Block from the Unblock of the measurement taken to determine the width shown in table 2. xb1 + xub1 = xf1 = 50.0cm = 52.5cm = 2.5 cm xb2 + xub2 = xf2 = 50.0cm = 52.5cm = 2.5 cm xf1 = 0.05 cm xf2 = 0.05 cm 2. To calculate the best estimates for the times it took the flag to pass at each gate the average of the 10 trials were taken using Excel. The averages were calculated to be as follows: tb1i = 0.069 s tb1f = 0.228 s tb2f = 0.057 s The standard deviation of the times was calculated in Excel to be as follows: σ tb1i = 0.000994s σ tb1f = 0.016028s σ tb2f = 0.000919s To find ∆tb the following formula was used tb 2 t ins 2 We know that ∆tins = 0.001s t b1i 0.0009942 0.0012 = 0.001410 s t b1 f 0.0160282 0.0012 = 0.016059 s t b 2 f 0.0009192 0.0012 = 0.001358 s 3. The velocity for each glider passing in the appropriate gate was calculated according to w the formula: vinst x . t 2.5 cm 36.23 v1i = 0.069 s 2.5 cm 10.96 v1f = 0.228 s 2.5 cm 43.86 v2f = 0.057 s 4. The uncertainty in velocity is given by the formula: v w 1 v v tb w = 2 tb + ∆w. tb tb w tb and calculated to be the following: cm 2.5 1 0.001410 0.1 = 2.1897 2 0.069 0.069 s cm 2.5 1 0.016059 0.1 = 1.2109 ∆v1f = 2 0.228 0.228 s cm 2.5 1 0.001358 0.1 = 2.7993 ∆v2f = 2 0.057 0.057 s ∆v1i = 5. The initial and final momentums were calculated according to the formulas: g cm cm = 14709 s s g cm cm cm Pf m1v1 f m2 v 2 f = 406 g * 10.96 + 205 g * 43.86 = 13441 s s s 6. The uncertainty in the initial momentum was calculated by the error propagation rule: Pi m1v1i = 406 g * 36.23 pi pi p m1 i v1i = v1i m1 m1 v1i m1 v1i And calculated to obtain the following result: g cm . s The uncertainty in the final momentum was calculated by the error propagation rule: pi = 36.23 0.5 406 2.1897 = 907 p f p f m1 m1 p f v1 f v1 f p f m2 m2 p f v2 f v2 f = v1 f m1 m1v1 f v2 f m2 m2 v2 f And calculated to be the following: p f = 10.96 * 0.5 + 406 * 1.2109 + 43.86 * 0.5 + 205 * 2.7993 = 1093 g cm s Fractional uncertainties were found to be as follows: ∆ Pi / Pi = 907 / 14709 = 0.06 ∆ Pf / Pf = 1093 / 13441 = 0.08 7. see conclusion 8. The Initial and final kinetic energies were calculated according to the following formulas: m1v12i 406 36.23 2 g cm 2 = = 266460 2 2 s2 m2 v22 f g cm 2 405 10.96 2 205 43.86 2 = = 221503 . 2 2 2 s2 Ki Kf m1v12f 2 9. The uncertainties in the initial kinetic energy were xcalculated using the error propagation rule: 2 v1i K i K i m1 m1v1i v1i K i m1 v1i = 2 m1 v1i and was calculated to obtain the following result: g cm 2 K i = 656 * 0.5 + 406 * 36.23 * 2.1897 = 32537 s2 The uncertainties in the final kinetic energy was calculated using the error propagation rule: K f K f Kf Kf K f m1 v1 f m2 v2 f = m1 v1 f m2 v2 f = v1 f 2 2 m1 m1v1 f v1 f v2 f 2 2 m2 m2 v2 f v2 f K f = 30.03 + 5388 + 480 + 28147 = 30694 Fractional uncertainties were found to be as follows: ∆ K i / K i = 32537 / 266460 = 0.12 ∆ K f / K f = 30694 / 221503 = 0.14 10. see conclusion g cm 2 s2 Part B 1. To calculate the best estimates for the times it took the flag to pass at each gate the average of the 10 trials were taken using Excel. The averages were calculated to be as follows: tb1i = 0.0693 s tb(1&2)f = 0.1137 s The standard deviation of the times was calculated in Excel to be as follows: σ tb1i = 0.000483s σ tb(1&2)f = 0.002791s To find ∆tb the following formula was used t b 2 tins 2 We know that ∆tins = 0.001s t b1i 0.0004832 0.0012 = 0.000493 s t b(1&2) f 0.0027912 0.0012 = 0.002965 s The velocity for the glider before the collision is given by v1 and after the collision by v2 was calculated according to the formula: w vinst x . t And found to be the following: 2.5 cm 36.08 v1 = 0.0693 s 2.5 cm 21.99 v2 = 0.1137 s The uncertainty in velocity is calculated using the formula derived in part A and found to be 1 w ∆v = 2 t b + ∆w. tb tb cm 2.5 1 0.000493 0.1 = 1.700 2 0.0693 s 0.0693 cm 2.5 1 0.002965 0.1 = 1.453 ∆v2 = 2 0.1137 0.1137 s ∆v1 = 2. The initial and final momentums were calculated according to the formulas: g cm cm = 14648 s s g cm cm Pf (m1 m2 )v 2 = (204+406) 21.99 = 13435 s s Pi m1v1 = (406) 36.08 The uncertainty in the momentum was calculated by the error propagation rule derived in part A and used to obtain the following results: g cm . pi v1 m1 m1 v1 = 36.08 0.5 406 1.700 = 708 s g cm p f v 2 m1 v 2 m2 (m1 m2 )v 2 = 21.99 0.5 36.08 0.5 6111.453 = 917 s Fractional uncertainties were found to be as follows: ∆ Pi / Pi = 708 / 14648= 0.048 ∆ Pf / Pf = 917 / 13435= 0.068 3. The Initial and final kinetic energies were calculated according to the following formulas: m v 2 406 36.08 2 g cm 2 = 264259 K i 1 1i = 2 2 s2 (m m2 )v 22 611 21.99 2 g cm 2 = = 147728 . Kf 1 2 2 s2 The Uncertainties in the initial and final kinetic energies were calculated using the error propagation rule: v1 g cm 2 m1 m1v1 v1i = 650.1 x 0.5 + 406 x 36.08 x 1.700 = 25227 2 s2 2 2 v2 v2 K f m1 m2 (m1 m2 )v 2 v 2 = 2 2 g cm 2 = 241.8 x 0.5 + 241.8 x 0.5 + 611 x 21.99 x 1.453= 19764 s2 2 K i Fractional uncertainties were found to be as follows: ∆ K i / K i = 25277/ 264259 = 0.10 ∆ K f / K f = 19764 / 147728= 0.13 Results Part A Velocity cm cm 2.1897 s s cm cm v1f = 10.96 1.2109 s s cm cm v2f = 43.86 2.7993 s s v1i = 36.23 Momentum g cm g cm . 907 s s g cm g cm P f 13441 1093 s s Pi 14709 Fractional Uncertainties: ∆ Pi / Pi = 0.06 ∆ Pf / Pf = 0.08 Kinetic Energy g cm 2 g cm 2 K i = 266460 32537 s2 s2 g cm 2 g cm 2 K f = 221503 30694 s2 s2 Fractional Uncertainties: ∆ K i / K i = 0.12 ∆ K f / K f = 0.14 Part B Velocity cm cm 1.700 s s cm cm v2 = 21.99 1.453 s s v1 = 36.08 Momentum g cm g cm . 708 s s g cm g cm Pf = 13435 917 s s Pi = 14648 Fractional Uncertainties: ∆ Pi / Pi = 0.048 ∆ Pf / Pf = 0.068 Kinetic Energy: g cm 2 g cm 2 K i 264259 25227 s2 s2 g cm 2 g cm 2 K f 147728 19764 s2 s2 Fractional Uncertainties: ∆ K i / K i = 0.10 ∆ K f / K f = 0.13 Conclusion For part A there was conservation of Momentum because Pi = 14709 907 Pf = 13441 1093 g cm . And s g cm . There is an intersection between the two values and therefore the s momentum is conserved. The kinetic energy is also conserved because K i = 266460 32537 g cm 2 g cm 2 K and = 221503 30694 . There is an intersection between the two values f s2 s2 and therefore kinetic energy is conserved. From both the conservation of momentum and kinetic energy we come to the conclusion that the collisions in part A were elastic collisions. For part B the Momentum was conserved because: Pi = 14648 708 13435 917 g cm and Pf = s g cm . There is an intersection between the two values and therefore the s momentum is conserved. The kinetic obtained was K i = 264259 25227 147728 19764 g cm 2 and K f = s2 g cm 2 . There is no intersection between the two answer sets and therefore s2 kinetic energy was not conserved. This proves that the collisions performed in part B are nonelastic and contrariwise.