9. For the table below, use the formula for Total Internal Reflection to predict what the critical angle will be. For th

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9. For the table below, use the formula for Total Internal Reflection to predict what the critical angle will be. For th

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9 For The Table Below Use The Formula For Total Internal Reflection To Predict What The Critical Angle Will Be For Th 1
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9. For the table below, use the formula for Total Internal Reflection to predict what the critical angle will be. For this calculation, use the average n value you previously determined and the appropriaten value isted in the table below. After doing so, set the index of refraction for the lower half matel (wer) to the appropriate value listed in the table below. Then determine the critical angle by moving the laser and finding the smallest angle (relative to the normal) at which no refraction occurs. This angle is the critical angle. Record it in the table below Prediction from Value from Power formula for en simulation for (degrees) (degrees) 25 Trial 11.02 Trial 2 1.27 Trial 3 1.59 PHET Part Questions Wie Rev
6. Determine the average nm & on. Additionally, determine the relative uncertain average nM= 2.52 average on=.098 relative uncertainty of average n = 3.9 7. Complete the statement below so that it is true. "My trial 3 8. Change the upper half material to Mystery A and change the lower half mater Bending Light value of nm was the most precise because its relative un 9. For the table below, use the formula for Total Internal Reflection to predict v in the table below. After doing so, set the index of refraction for the lower h the smallest angle (relative to the normal) at which no refraction occurs. Th Trial 1 1.02 Trial 2 1.27 Trial 3 1.59 Prediction from Value from njower formula for crit simulation for crit (degrees) (degrees) Part B: Questions PHET= 25
Introduction For this lab you will use the simulation below to investigate Snell's Law & Total Internal Reflection. esc Ray O Wave Normal Bending Light * F1 TIT 60 90 60 F2 30 30 0 ETT 30 80 F3 30 60 90 60. Intro Prisms More Tools 000 000 F4 MA FS Material Mystery A What is n? Material Custom Index of Refraction (n) Air Water F6 MacBook Air 1.02 Glass PHET = F7 DII FB
5. Fill in the table below by using the Index of Refraction slider to set the index of refraction (n) for the upper half material to the values in the table below, record the angle of refraction (u), and then use Snell's Law to calculate the index of refraction for Mystery A (nu). To determine the uncertainty of that calculation (), use the formula shown above the table on the left. Additionally, determine the relative uncertainty of each ny by using the formula above the table on the right. The relative uncertainty lets you know how precise your value is (smaller is better). op HR / 1 180 + tình tan PM (degrees) n Trial 1 1.19 25 Trial 2 1.38 30 Trial 3 1.59 35 ✓2.55 2.5 2.51 relative uncertainty x 100 AM TIM 116 096 083 7. Complete the statement below so that it is true. "My trial 3 relative uncertainty of n (96) 4.55 3.84 3.31 6. Determine the average ny & Additionally, determine the relative uncertainty of the average ny average ny-2.52 average 098 relative uncertainty of average n-3.9 value of n was the most precise because its relative uncertainty was the lowest
8. Change the upper half material to Mystery A and change the lower half material to Air. After doing so, it should look like the screenshot below. Notice that total internal reflection is occurring. PHET 9. For the table below, use the formula for Total Internal Reflection to predict what the critical angle will be. For this calculation, use the average n value you previously determined and the appropriate in value listed in the table below. After doing so, set the index of refraction for the lower half material (Power to the appropriate value listed in the table below. Then determine the critical angle by moving the laser and finding the smallest angle (relative to the normal) at which no refraction occurs. This angle is the critical angle. Record it in the table below. Prediction from Value from Tower formula for font simulation for fort (degrees) (degrees) Trial 1 1.02 00 Trial 2 1.27 Trial 3 1.59
9. For the table below, use the formula for Total Internal Reflection to predict in the table below. After doing so, set the index of refraction for the lower the smallest angle (relative to the normal) at which no refraction occurs. T Prediction from Value from nlower formula for crit simulation for crit (degrees) (degrees) Trial 1 1.02 Trial 2 1.27 Trial 3 1.59 90 X
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