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- Using the information given in Table 10.4, determine the ratio of local pressure and density to sea-level values. Estimate the value of air density at the cruising altitude of most commercial airliners. Altitude (m) sealevel PPsealevel 0 (sea level) 1000 3000 5000 8000 10,000 12,000 14,000 15,000An astronaut has a mass of 68 kg. What is the weight of the astronaut on Earth at sea level? What are the mass and the weight of the astronaut on the Moon, and on Mars? What is the ratio of the pressure exerted by the astronauts shoe on Earth to Mars?Pitot PipeBy connecting a mercury pressure gauge to a vertical pipeline through which water is transmitted, speed measurement is performed with a pitot tube. Since the deviation from the pressure gauge column is 15 cm, calculate the speed of the water in the pipe. (Pmercury=13560 kg/m3, Pwater=1000 kg/m3) (Answer is V2=6.08 m/s)
- 1. In calibrating a 10-mL pipet, a measured volume of water was transferred to a tared flask and weighed, yielding a mass of 9.9814 g. (a) Calculate, with and without correcting for buoyancy, the volume of water delivered by the pipet. Assume that the density of water is 0.99707 g/cm3 and that the density of the weights is 8.40 g/cm3. (b) What are the absolute and relative errors introduced by failing to account for the effect of buoyancy? Is this a significant source of determinate error for the calibration of a pipet? Explain. 2. Repeat the questions in problem 1 for the case when a mass of 0.2500 g is measured for a solid that has a density of 2.50 g/cm3. 3. Is the failure to correct for buoyancy a constant or proportional source of determinate error?4. The water in a tank on the right is pressurized by air, and the pressure is measured by a multifluid manometer as shown in figure. Determine the gage pressure (kPa) of air in the tank if h₁ = 0.4 m, h2 = 0.6 m, and h3 = 0.8 m. Take the densities of water, oil, and mercury to be 1000 kg/m³, 850 kg/m³, and 13,600 kg/m³, respectively. (2 decimal)Calculate the capillary effect in millimeters in a glass tube of 4mm diameter, when immersed in Water Mercury the temperature of the liquid is 200C in contact with air are 0.073575 N/m and 0.51 N/m respectively. The angle of contact for water is zero and that for mercury is 1300. Take density of water at 200C as equal to 998 kg/m3. Explain the ways of describing the fluid motion
- Refer to the flow shown in the figure. The velocity before the contraction is 1.51m/s. Given: h=0.20m D1=0.103m D2=0.057m Determine the height of the fluid in the manometer, H, in metersFluid Mechanics: (a) Convert a pressure head of 4.60 m of water to meters of oil, s.g. 0.750. (b) Convert a pressure head of 24 in of mercury to feet of oil, s.g. 0.750.Fluid Mechanics question: A device used for measuring the specific weight of a liquid consists of a u-tube manometer as shown. The manometer tube has an internal diameter of 0.5 cm and originally has water in it. Exactly 2 cm3 of unknown liquid is poured into one leg of the manometer, and a displacement of 5cm is measured between the surfaces as shown. What is the specific weight of the unknown liquid?
- As shown in the figure, water flows in the horizontal pipe. The pipe consists of two different sections, 60 mm and 30 mm in diameter, connected by a smooth reduction. The pressure difference between the two sections is measured with a mercury manometer. Friction effects are neglected. The height between the mercury levels in the two sections of the pipe was determined as 1.4m. Find the velocity and mass flow at points 1 and 2. (Density of mercury: 13.6 grams / cm3, Density of water: 1gr / cm3)fluıd mechanıcs If an oil tank is pulled uphill on a surface that makes an angle of 162 with the horizontal, the oil makes an angle of 160,a) Show the forces acting on the tank on the figure. Write the balance of force.b) Calculate the constant acceleration of the tank being pulled uphill.