Concept explainers
(a)
Find the principal moment of inertia at the origin O.
(a)

Answer to Problem 9.179P
The principal moment of inertia at the origin O is
Explanation of Solution
Given information:
The mass of the cylinder is denoted by m.
The length of the circular cylinder is denoted by a.
The diameter OB of the top surface makes
Calculation:
Show the homogeneous circular cylinder as shown in Figure 1.
Refer Figure 1.
Refer Figure 9.28.
Apply parallel axis theorem
Show the moment of inertia of the circular cylinder about the y axis as follows:
Show the moment of inertia of the circular cylinder about the x and z axis as follows:
Here, a is the radius of the cylinder and L is the length of the cylinder.
Substitute
The centroidal axis products of inertia are zero due to symmetry.
Write the centroidal locations as measured from the origin O along the x, y and z axis as below;
Express the moment of inertia
Express the moment of inertia
Express the moment of inertia
Show the Equation 9.56 as follows:
Substitute
Substitute
Solve the above Equation and get the values of
Show the principal moment of inertia as follows:
Thus, the principal mass moment of inertia are
(b)
Find the angles made by the principal axis of inertia at O with the coordinate axis.
(b)

Answer to Problem 9.179P
The angles made by the principal axis of inertia at O with the coordinate axis is
Explanation of Solution
Given information:
Consider the direction cosines of each principal axis are denoted by
Calculation:
Refer Part (a).
Show the Equation 9.54 as follows:
Substitute
Modify Equation (3).
Consider
Solve Equation (4).
Add both the Equation in Equation (4).
Substitute
Show the Equation 9.57 as follows:
Substitute
Consider K1.
Substitute
Calculate the value of
Substitute
Show the direction cosines
Conisder K3.
Substitute
Calculate the value of
Substitute
Show the direction cosines
Consider K2.
Show the Equation 9.54b as follows:
Substitute
Refer Equation (3) and (6).
Substitute
Modify above Equations as follows:
Solve Equation (8) and get the value of
Show the Equation 9.57 as follows:
Substitute
Show the direction cosines
Thus, the velocity of the point B is
(c)
Sketch the body and show the orientation of the principal axis of inertia relative to x, y, and z axis.
(c)

Explanation of Solution
Given information:
Calculation:
Refer Part (a) and (b).
Sketch the body and show the orientation of the principal axis of inertia relative to x, y, and z axis as shown in Figure 2.
Refer Figure 2.
The principal axis 1 and 3 lies on the vertical plane of symmetry passing through OB.
The principal axis 2 lies in xz plane.
Want to see more full solutions like this?
Chapter 9 Solutions
VECTOR MECHANIC
- A 23-ft3 rigid tank initially contains saturated refrigerant-134a vapor at 160 psia. As a result of heat transfer from the refrigerant, the pressure drops to 50 psia. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Determine the final temperature. Use data from refrigerant tables. The final temperature is ºF.arrow_forwardA 23-ft3 rigid tank initially contains saturated refrigerant-134a vapor at 160 psia. As a result of heat transfer from the refrigerant, the pressure drops to 50 psia. NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. Determine the heat transfer. The heat transfer is Btu.arrow_forwardThe shaft shown in the figure below is subjected to axial loads as illustrated. The diameters of segments AB, BC, and CD are 20mm, 25mm, and 15mm, respectively. If the modulus of elasticity of the material is 610 MPa. Determine the change of A to D lengtharrow_forward
- Determine the final pressure and temperature. The final pressure is kPa. The final temperature is ºC.arrow_forwardAir enters the 1-m2 inlet of an aircraft engine at 100 kPa and 20°C with a velocity of 184 m/s. Determine the volume flow rate, in m3/s, at the engine’s inlet and the mass flow rate, in kg/s, at the engine’s exit. The gas constant of air is R = 0.287 kPa·m3/kg·K. The volume flow rate at the engine’s inlet m3/s. The mass flow rate at the engine’s exit is kg/s.arrow_forwardThe ventilating fan of the bathroom of a building has a volume flow rate of 33 L/s and runs continuously. If the density of air inside is 1.20 kg/m3, determine the mass of air vented out in one day. The mass of air is kg.arrow_forward
- A steady-flow compressor is used to compress helium from 15 psia and 70°F at the inlet to 200 psia and 600°F at the outlet. The outlet area and velocity are 0.01 ft2 and 100 ft/s, respectively, and the inlet velocity is 53 ft/s. Determine the mass flow rate and the inlet area. The gas constant of helium is R = 2.6809 psia·ft3/lbm·R. The mass flow rate is lbm/s. The inlet area is ft2.arrow_forward1. The maximum and minimum stresses as well as the shear stress seen subjected the piece in plane A-A. Assume it is a cylinder with a diameter of 12.7mm 2. Draw the Mohr circle for the stress state using software. 3. Selection of the material for the prosthesis, which must be analyzed from the point of safety and cost view.arrow_forwardMarrow_forward
- × Your answer is incorrect. (Manometer) Determine the angle 0 of the inclined tube shown in figure below if the pressure at A is 1 psi greater than that at B. 1ft SG=0.61 十 A Ꮎ 1ft SG=1.0 8.8 ft 0 = Hi 15.20 deg Airarrow_forwardI don't know how to solve thisarrow_forward1. The maximum and minimum stresses as well as the shear stress seen subjected the piece in plane A-A. Assume it is a cylinder with a diameter of 12.7mm 2. Draw the Mohr circle for the stress state using software. 3. Selection of the material for the prosthesis, which must be analyzed from the point of safety and cost view.arrow_forward
- International Edition---engineering Mechanics: St...Mechanical EngineeringISBN:9781305501607Author:Andrew Pytel And Jaan KiusalaasPublisher:CENGAGE L
