Tutorials in Introductory Physics
Tutorials in Introductory Physics
1st Edition
ISBN: 9780130970695
Author: Peter S. Shaffer, Lillian C. McDermott
Publisher: Addison Wesley
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Chapter 12.1, Problem 4cT

A syringe is used to remove some water from the left side of the U-tube. The water level on the left side is seen to be lowered, butthe water level on the right does not change.

Chapter 12.1, Problem 4cT, A syringe is used to remove some water from the left side of the U-tube. The water level on the left

Consider the following student dialogue:

    Student 1: “The pressure at point F must now be higher than atmospheric pressure because the water there is being pushed up against the stopper.”
    Student 2: “I think that the pressure at point E must be the same as at point A because they are at the same level. These points are both at atmospheric pressure. So the pressure at point F is lower than atmospheric pressure because know that pressure gets less as you go up.”
    Student 3: “But water is more dense than air so the pressure at F cannot be less than atmospheric pressure.”

With which student(s), if any, do you agree?

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A pitot tube (the figure) is used to determine the airspeed of an airplane. It consists of an outer tube with a number of small holes B (four are shown) that allow air into the tube; that tube is connected to one arm of a U-tube. The other arm of the U-tube is connected to hole A at the front end of the device, which points in the direction the plane is headed. At A the air becomes stagnant so that vA = 0. At B, however, the speed of the air presumably equals the airspeed B of the plane.A pitot tube on a high-altitude aircraft measures a differential pressure of 230 Pa. What is the aircraft's airspeed if the density of the air is 0.0320 kg/m3?
A pitot tube (the figure) is used to determine the airspeed of an airplane. It consists of an outer tube with a number of small holes B (four are shown) that allow air into the tube; that tube is connected to one arm of a U-tube. The other arm of the U-tube is connected to hole A at the front end of the device, which points in the direction the plane is headed. At A the air becomes stagnant so that và = 0. At B, however, the speed of the air presumably equals the airspeed B of the plane. A pitot tube on a high-altitude aircraft measures a differential pressure of 240 Pa. What is the aircraft's airspeed if the density of the air is 0.0330 kg/m³? Number Pair- Hole A B B Units Liquid Air h
CO-3,4,5 SITUATION 4. (Flow in Pipes - a) A circular pipe has a diameter of 750 millimeters is flowing full of water. Diameter = D NOTES: For "Manning's Formula" Velocity V = 1/n x R S 2/3 1/2 d) WS O NOTES: Manning's Roughness Coef. n = 0.012 Consider pipe is flowing full. Pipe Invert Slope is S=1.55% Hydraulic Radius R= D/4 Flow Rate Q = A x V Figure 1. FLOW IN PIPES H +D Note: Volume = 1.0 m³ = 1,000 liters Calculate its hydraulic radius, R = ? in meters Calculate the mean velocity V = ? in meters per sec. Determine the flow rate Q = ? in cubic meters per sec. ? Determine the flow rate Q = ? in liters per sec. ?
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