Around 1870, Fred Goldsmith threw a baseball a couple degrees to his right of the pitcher. What happened next was a phenomenon known as the curve ball. The ball curved back to the left, directly in front of the pitcher. Where is the air pressure the lowest on the ball as it travels towards the pitcher?
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- A new gel is being developed to use inside padding and helmets to cushion the body from impacts. The gel is stored in a 4.9 cubic meters [m] cylindrical tank with a diameter of 2 meters [m]. The tank is pressurized to 1.3 atmosphere [atm] of surface pressure to prevent evaporation. A total pressure probe located at the bottom of the tank reads 57 feet of water [ft H, 0]. What is specific gravity of the gel contained in the tank?A submarine is designed for depths to 1500 m. What is the maximum pressure diOfference between the submarine's interior maintained at normal atmospheric pressure and the surrounding? * O 3.5 x 10^(7) Pa 4.5 x 10^(7) Pa O 2.3 x 10^(7) Pa O 1.5 x 10^(7) PaThe top of a treasure chest lies 10.8 m below the surface of Lake Ontario. What is the absolute pressure (in Pa) acting on the top of the chest
- Your office has a 0.025 m^3 cylindrical container of drinking water. The radius of the container is about 14 cm. When the container is full, what is the gauge pressure that the water exerts on the sides of the container halfway down from the top? When the container is full, what is the gauge pressure that the water exerts on the sides of the container all the way down from the top?A large spherical air balloon is filled with helium. If the balloon is to support (meaning produce a net acceleration of 0) a total load of 300 kg, including its own mass, calculate the minimum radius of the balloon. Assume values of the density of air and helium to be 1.29 kg/m and 0.18 kg/m respectively 4.8 m 3.6 m O 3.8 m O 3.1 m O 4.5 mP=0 at the top of the vertical tube.
- A Venturi meter is a device for measuring the speed of a fluid within a pipe. The drawing shows a gas flowing at speed v2 through a horizontal section of pipe whose cross-sectional area is A2 = 0.0937 m2. The gas has a density of ρ = 1.30 kg/m3. The Venturi meter has a cross-sectional area of A1 = 0.0234 m2 and has been substituted for a section of the larger pipe. The pressure difference between the two sections is P2 - P1 = 149 Pa. Find (a) the speed v2 of the gas in the larger original pipe and (b) the volume flow rate Q of the gas. I posted it just now and recieved the wrong answers so i'm asking again. The answers are not A) 1.87 and B) 0.157.As the summer intern for a company that manufactures nozzles for garden hoses, you are working on an adjustable hose nozzle project. Your design calls for a rotating head that has a number of cylindrical plugs that can be inserted into the hose opening. On a particular setting, the speed of the water passing around the plug is 9 times as large as the speed of the water in the hose. Determine the ratio of the plug radius (rplug) to the inside hose radius (/hose). plug = ThoseAs the summer intern for a company that manufactures nozzles for garden hoses, you are working on an adjustable hose nozzle project. Your design calls for a rotating head that has a number of cylindrical plugs that can be inserted into the hose opening. On a particular setting, the speed of the water passing around the plug is 5 times as large as the speed of the water in the hose. Determine the ratio of the plug radius (rplug) to the inside hose radius (r hose).
- A tank holds a large amount of water. A pipe is connected to the tank at the upper end and is open to the air at the lower end (see figure).The upper end of the pipe is h1 = 1.90-m above the ground. The lower end of the pipe is h2 = 0.570-m above the ground. The water at the upper end of the pipe has a speed of 0.640 m/s. The water at the lower end of the pipe has a speed of 8.50 m/s.What is the pressure in the water in the pipe at the upper end of the pipe?The air above an airplane wing moves faster than the air below it. A certain airplane wing has an area of 124m^2. The wind speed above the wing is 258m/s and below it is 220m/s. Assuming that the elevation and air density (1.23kg/m^3) are approximately the same at these two points, what is the pressure difference caused by the wind speeds? What is the lift force on the wing?You may find it helpful to review Chapter 9, Section 9.3 "Fluid flow measurements" and Chapter 11, Section 11.1 "The Earth's atmosphere and winds" before attempting this question. An aircraft is flying at an altitude of 31000 feet at a speed of 450 knots. What pressure difference will be produced with a pitot-static probe at this height and speed? Give your answer in kPa to 2 s.f. (Even if this question might be answered using either equations or graphs, use equations only to provide a more accurate result.) Suggested approach: Remember that the local air density at 31000 feet is less than the value at ground level, and find this value first. Use the standard atmospheric model and assume that 1 foot = 0.305m and 1 knot = 0.514 m s¹. Pressure difference: kPa