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Problem 17–82 | Internal Normal Force, Shear Force & Moment at Section A | Chapter 17 Dynamics
Problem 17–82 | Internal Normal Force, Shear Force & Moment at Section A | Chapter 17 Dynamics
Problem 17–82 The lightweight turbine consists of a rotor which is powered from a torque applied at its center. At the instant the rotor is horizontal it has an angular velocity of 15 extrad/s and a clockwise angular acceleration of 8 extrad/s
2
. Determine the internal normal force, shear force, and moment at a section through A. Assume the rotor is a 50-m-long slender rod, having a mass of 3 extkg/m.
In this problem, we analyze the internal loading in a rotating slender rod using planar rigid body kinetics and section-cut force/moment analysis.
The solution is presented in a clear, step-by-step manner and includes:
Identifying the rotor as a uniform slender rod of length 50 m with distributed mass 3 extkg/m.
Computing the total mass and locating the mass center of the rotor.
Determining the acceleration of material points due to rotation and angular acceleration.
Separating acceleration into tangential and normal components for points along the rod.
Drawing the free-body diagram of the portion of the rotor cut at section A.
Applying
Newton’s second law in the normal direction
to determine the internal normal force at the section.
Applying
Newton’s second law in the tangential direction
to determine the internal shear force.
Applying the rotational equation of motion about the section to determine the internal bending moment.
Interpreting the physical meaning of axial loading, shear transfer, and bending in the rotating rotor.
Key concept
The normal force is associated primarily with the centripetal acceleration distribution, the shear force is associated with tangential acceleration from α, and the internal moment comes from the distributed inertial loading acting on the cut segment.
This problem is essential for understanding how rotating members develop internal forces and moments under combined angular velocity and angular acceleration.
This video is especially useful for:
Engineering Mechanics – Dynamics
Rigid Body Kinetics
Distributed Inertial Loading
Internal Force and Moment Analysis
Slender Rod Dynamics
Exam and Homework Preparation
Keywords
engineering mechanics dynamics, internal normal force, internal shear force, internal moment calculation, rotating slender rod, rotor dynamics, rigid body kinetics, distributed inertial loading, angular velocity and angular acceleration, Newton Euler equations, section cut analysis, centripetal acceleration effects, tangential acceleration effects, chapter 17 dynamics solutions, mechanical engineering dynamics, engineering mechanics solved problems, Hibbeler dynamics solutions, rigid body rotation, bending moment in rotating member, exam oriented dynamics problems, turbine rotor internal forces
#Dynamics #EngineeringMechanics #RigidBodyKinetics #RotorDynamics #InternalForces #InternalMoment #NewtonEuler #MechanicalEngineering #HibbelerDynamics #Chapter17 #ExamPreparation
Видео Problem 17–82 | Internal Normal Force, Shear Force & Moment at Section A | Chapter 17 Dynamics канала NUM
Problem 17–82 The lightweight turbine consists of a rotor which is powered from a torque applied at its center. At the instant the rotor is horizontal it has an angular velocity of 15 extrad/s and a clockwise angular acceleration of 8 extrad/s
2
. Determine the internal normal force, shear force, and moment at a section through A. Assume the rotor is a 50-m-long slender rod, having a mass of 3 extkg/m.
In this problem, we analyze the internal loading in a rotating slender rod using planar rigid body kinetics and section-cut force/moment analysis.
The solution is presented in a clear, step-by-step manner and includes:
Identifying the rotor as a uniform slender rod of length 50 m with distributed mass 3 extkg/m.
Computing the total mass and locating the mass center of the rotor.
Determining the acceleration of material points due to rotation and angular acceleration.
Separating acceleration into tangential and normal components for points along the rod.
Drawing the free-body diagram of the portion of the rotor cut at section A.
Applying
Newton’s second law in the normal direction
to determine the internal normal force at the section.
Applying
Newton’s second law in the tangential direction
to determine the internal shear force.
Applying the rotational equation of motion about the section to determine the internal bending moment.
Interpreting the physical meaning of axial loading, shear transfer, and bending in the rotating rotor.
Key concept
The normal force is associated primarily with the centripetal acceleration distribution, the shear force is associated with tangential acceleration from α, and the internal moment comes from the distributed inertial loading acting on the cut segment.
This problem is essential for understanding how rotating members develop internal forces and moments under combined angular velocity and angular acceleration.
This video is especially useful for:
Engineering Mechanics – Dynamics
Rigid Body Kinetics
Distributed Inertial Loading
Internal Force and Moment Analysis
Slender Rod Dynamics
Exam and Homework Preparation
Keywords
engineering mechanics dynamics, internal normal force, internal shear force, internal moment calculation, rotating slender rod, rotor dynamics, rigid body kinetics, distributed inertial loading, angular velocity and angular acceleration, Newton Euler equations, section cut analysis, centripetal acceleration effects, tangential acceleration effects, chapter 17 dynamics solutions, mechanical engineering dynamics, engineering mechanics solved problems, Hibbeler dynamics solutions, rigid body rotation, bending moment in rotating member, exam oriented dynamics problems, turbine rotor internal forces
#Dynamics #EngineeringMechanics #RigidBodyKinetics #RotorDynamics #InternalForces #InternalMoment #NewtonEuler #MechanicalEngineering #HibbelerDynamics #Chapter17 #ExamPreparation
Видео Problem 17–82 | Internal Normal Force, Shear Force & Moment at Section A | Chapter 17 Dynamics канала NUM
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12 июня 2026 г. 12:00:37
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