Calculating Pressure Difference in a Manometer with Oil/Mercury

AI Thread Summary
The discussion focuses on calculating the fluid level rise in a manometer connected to an air tank when the pressure increases by 0.75 cm of Hg. The initial calculations using oil with a density of 0.9 g/cm³ yielded a rise of 1.1326 cm and a final pressure of 1.9821 cm, leading to confusion over the difference. The key point is that the pressures must balance, and the oil column only rises to half the height due to the opposing movements on either side of the manometer. If mercury were used instead, the calculations would differ significantly due to its higher density. Accurate pressure balance is essential for determining the correct fluid level rise in both scenarios.
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A manometer using oil (density 0.9 g/cm3) as a fluid is connected to an air tank. Suddenly the pressure in the tank increases by 0.75 cm of Hg. (a) By how much does the fluid level rise in the side of the manometer that is open to the atmosphere? (b) What would your answer be if the manometer used mercury instead?

I'm using 1 Pa for initial pressure and 1.75 Pa for final pressure

1 = .0009kg/cm^3(981 cm/s^2)(d) =>1.1326cm
1.75 = .0009kg/cm^3(981 cm/s^2)(d) =>1.9821cm

1.9821-1.1326 = .8495cm - this is wrong? any ideas why?
 
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The two pressures need to balance each other - the pressures of the stated mercury column (rise in the pressure in the tank) and the pressure of the raised oil column. But the oil column will only rise to only half the balancing height due to the fact that on the tank side it lowers by half the height and on the open side it rises by the other half.
 
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