This document contains the homework submission of student Tran Quoc Thai for the Engineering Mechanics course. It includes 6 problems solving statics analysis of different structures. The student provides the free body diagrams, equilibrium equations, and solutions for the support reactions and internal forces of each structure when subjected to various loads.
The document discusses the deformation of beams due to bending. It recaps previous discussions on shear force and bending moment distributions, and normal and shear stress distributions. It then introduces the concept of determining deflections and slopes of beams under load using differential equations. The document provides the assumptions made in the analysis, such as neglecting shear deformation. It then derives the relationship between moment and curvature using small angle approximations. Finally, it presents an example problem to demonstrate solving the differential equation for deflection using appropriate boundary conditions.
1. The document discusses vibration analysis of single degree of freedom (SDOF) systems subjected to earthquake loading.
2. It covers various topics including free vibration of undamped and damped SDOF systems, response to harmonic and arbitrary loading, and multi degree of freedom systems.
3. The key equations of motion for free vibration, damped vibration, and forced vibration under harmonic loading are presented. Solution methods such as normal mode analysis and response history analysis are also introduced.
The document discusses the deformation of beams due to bending. It recaps previous discussions on shear force and bending moment distributions, and normal and shear stress distributions. It then introduces the concept of determining deflections and slopes of beams under load using differential equations. The document provides the assumptions made in the analysis, such as neglecting shear deformation. It then derives the relationship between moment and curvature using small angle approximations. Finally, it presents an example problem to demonstrate solving the differential equation for deflection using appropriate boundary conditions.
1. The document discusses vibration analysis of single degree of freedom (SDOF) systems subjected to earthquake loading.
2. It covers various topics including free vibration of undamped and damped SDOF systems, response to harmonic and arbitrary loading, and multi degree of freedom systems.
3. The key equations of motion for free vibration, damped vibration, and forced vibration under harmonic loading are presented. Solution methods such as normal mode analysis and response history analysis are also introduced.
JEE Mathematics/ Lakshmikanta Satapathy/3D Geometry theory part 9/ Equation of plane in intercept form and plane passing through the line of intersection of two planes
This document discusses power flow analysis and the Newton-Raphson power flow method. It provides details on setting up the power flow problem, including defining the power balance equations in terms of real and reactive power. It also describes calculating the Jacobian matrix and differentiating the power flow equations to populate the matrix. An example power flow case is presented on a two bus system to illustrate applying the Newton-Raphson method through multiple iterations to solve for the voltage magnitude and angle.
This document provides detailed solutions to the 2013 JEE Advanced Paper 1 with code 0. It contains solutions to 10 multiple choice questions in Section 1 and 5 multiple choice questions in Section 2 of the Physics portion of the exam. The solutions explain the conceptual reasoning and calculations for arriving at the correct answers. Key details provided in the solutions include relevant equations, diagrams, and step-by-step working.
1. The document describes the process of load flow analysis using the Newton-Raphson power flow method.
2. The Newton-Raphson power flow method uses Newton's method to solve the nonlinear power balance equations to determine the voltage magnitude and angle at each bus in the power system.
3. It derives the real and reactive power balance equations, defines the power flow variables, describes calculating the Jacobian matrix and its elements, and provides an example of applying the method to a two bus system to solve for the unknown voltage magnitude and angle at the second bus.
1. The document provides instructions to solve problems related to digital waveguide oscillators, digital lattice filters, and other discrete-time linear systems. Students are asked to write state space equations, find eigenvalues, compute responses, and represent systems using different forms such as state space and block diagrams. MATLAB code is provided to help with computations.
2. Students must analyze cascaded and parallel systems, check controllability and observability, and represent pulse transfer functions using state space, direct form, cascade form, and other block diagram representations. They are also asked to transform state space representations between different coordinate systems.
The document discusses equilibrium of particles and coplanar force systems. It has the following key points:
1) It introduces concepts of equilibrium, free body diagrams, and equations of equilibrium (scalar and vector forms) for solving 2D and 3D static equilibrium problems.
2) Examples are provided to demonstrate drawing free body diagrams and using the equations of equilibrium to solve for unknown forces in 2D and 3D systems involving cables, pulleys, springs, and other mechanics elements.
3) Procedures are outlined for setting up and solving static equilibrium problems involving both 2D coplanar and 3D non-coplanar force systems.
The document provides information about the format and marking scheme of the JEE (Advanced) exam from 2013, including:
- The exam has 3 parts (Physics, Chemistry, Mathematics) with 3 sections each: multiple choice with single correct answer, multiple choice with one or more correct answers, and questions with single-digit answers.
- Sections 1 and 3 award marks for correct answers and deduct marks for incorrect answers. Section 2 awards marks only for fully correct answers and deducts marks otherwise.
- An example question is provided for Section 1 of the Physics part of the exam.
The document discusses determining the angle between two lines and finding the point of intersection between two lines in 3D space. It provides the equations and process for finding the angle between two lines given their direction ratios. It also outlines the steps to find the point of intersection, which involves setting the coordinates of a point on each line equal to determine values for lambda and mu, and substituting those values back into one of the line equations. An example problem demonstrates finding the intersection point of two lines.
This document discusses statically indeterminate beams and methods for solving them. It begins by recapping free body diagrams, equilibrium, displacement compatibility, and force-displacement relations. It then introduces the procedure for solving statically indeterminate problems using the method of integration or method of superposition. Examples are provided to demonstrate applying these methods, including drawing free body diagrams, writing equilibrium equations, determining compatibility equations using boundary conditions, formulating moment equations, and integrating to find displacement equations. Key steps like determining constants of integration and unknown reactions using boundary conditions are shown. Finally, some remarks are made about accounting for shear and axial deformation in displacement calculations.
This document provides an overview of coplanar non-concurrent force systems and methods for analyzing them. It defines key terms like resultant, equilibrium, and equilibrant. Examples are provided to demonstrate determining resultants and support reactions for coplanar force systems, beams under different loading conditions, and plane trusses. Methods like Lami's theorem, free body diagrams, and the principles of equilibrium are used to solve for unknown forces. Truss analysis is also briefly discussed, noting trusses are articulated structures carrying loads at joints, with members in axial tension or compression.
Iit jam 2016 physics solutions BY TrajectoryeducationDev Singh
1. The electric field at a point (a, b, 0) due to an infinitely long wire with uniform line charge density λ is given by E=λ/(2πε0)(a/r2)ex+(b/r2)ey, where r2=a2+b2.
2. For a 1W point source emitting light uniformly in all directions, the Poynting vector at the point (1, 1, 0) is 1/(8π)ex+(y/e)ey W/cm2.
3. A charged particle starting from the origin with velocity 3/2ex+2ez m/s in a uniform magnetic field B=B
Deflection of structures using double integration method, moment area method, elastic load method, conjugate beam method, virtual work, castiglianois second theorem and method of consistent deformations
This module discusses coordinate proofs and properties of circles on the coordinate plane. It introduces coordinate proofs as an analytical method of proving geometric theorems by using the coordinates of points and algebraic relationships. Examples demonstrate proving properties of triangles and quadrilaterals analytically. The standard form of the equation of a circle is derived from the distance formula as (x - h)2 + (y - k)2 = r2, where (h, k) is the center and r is the radius. Finding the center, radius, and equation of circles in various forms are illustrated.
The document discusses the Newton-Raphson power flow method for solving power systems. Some key points:
- Newton-Raphson is commonly used for power flow analysis due to its fast convergence when initial guesses are close to the solution and large region of convergence. However, each iteration takes longer than Gauss-Seidel and it is more complicated to code.
- It uses Newton's method to determine the voltage magnitude and angle at each bus that satisfies the power balance equations. The power flow Jacobian matrix is calculated by differentiating the real and reactive power balance equations with respect to the voltage variables.
- A two-bus example demonstrates setting up and solving the power flow problem using Newton-Raphson
Determinants provide a scalar quantity associated with square matrices. There are several properties of determinants, including that the determinant of a matrix does not change if rows or columns are interchanged. The determinant can be expressed as the sum of the products of each element and its corresponding cofactor. Examples show how to evaluate determinants by expanding along rows or columns and applying properties such as identical rows resulting in a determinant of zero.
Determinants provide a scalar quantity associated with square matrices. There are several properties of determinants, including that the determinant of a matrix does not change if rows or columns are interchanged. The determinant can be expressed as the sum of the products of each element and its corresponding cofactor. Examples show how to evaluate determinants by expanding along rows or columns and applying properties such as identical rows resulting in a determinant of zero.
This document contains instructions for 12 math problems involving solving quadratic equations through various methods like factorization, using the quadratic formula, completing the square, and solving simultaneous linear equations and inequalities. Learners are asked to solve quadratic equations, determine if expressions are quadratic, factorize expressions, find the solution set of inequalities, and solve absolute value equations.
This document provides an overview of statics concepts including:
- Forces on particles in 2D and 3D space including addition and resolution of forces
- Equilibrium of particles and rigid bodies using free body diagrams
- Moments of forces about points and axes
- Force couples and equivalent force systems
- Example problems are provided to demonstrate applying concepts to determine tensions, components of forces, moments, and equivalent single forces.
1. The document discusses concepts related to force system resultants including cross products, moments of forces, and principles of moments.
2. It provides definitions and formulas for calculating the cross product of two vectors, the moment of a force about a point, and the resultant moment of a system of forces.
3. Examples are given to demonstrate calculating moments of forces using vector and scalar methods for different axis orientations.
This document outlines key concepts in 2D and 3D force systems. It begins by defining forces and force components in rectangular coordinate systems. It discusses concepts like concentrated vs distributed forces, and contact vs body forces. It also covers moments, couples, and resultants of force systems. Several example problems are provided to demonstrate calculating forces, moments, and resultants for 2D systems.
GraphSummit Singapore | The Art of the Possible with Graph - Q2 2024Neo4j
Neha Bajwa, Vice President of Product Marketing, Neo4j
Join us as we explore breakthrough innovations enabled by interconnected data and AI. Discover firsthand how organizations use relationships in data to uncover contextual insights and solve our most pressing challenges – from optimizing supply chains, detecting fraud, and improving customer experiences to accelerating drug discoveries.
JEE Mathematics/ Lakshmikanta Satapathy/3D Geometry theory part 9/ Equation of plane in intercept form and plane passing through the line of intersection of two planes
This document discusses power flow analysis and the Newton-Raphson power flow method. It provides details on setting up the power flow problem, including defining the power balance equations in terms of real and reactive power. It also describes calculating the Jacobian matrix and differentiating the power flow equations to populate the matrix. An example power flow case is presented on a two bus system to illustrate applying the Newton-Raphson method through multiple iterations to solve for the voltage magnitude and angle.
This document provides detailed solutions to the 2013 JEE Advanced Paper 1 with code 0. It contains solutions to 10 multiple choice questions in Section 1 and 5 multiple choice questions in Section 2 of the Physics portion of the exam. The solutions explain the conceptual reasoning and calculations for arriving at the correct answers. Key details provided in the solutions include relevant equations, diagrams, and step-by-step working.
1. The document describes the process of load flow analysis using the Newton-Raphson power flow method.
2. The Newton-Raphson power flow method uses Newton's method to solve the nonlinear power balance equations to determine the voltage magnitude and angle at each bus in the power system.
3. It derives the real and reactive power balance equations, defines the power flow variables, describes calculating the Jacobian matrix and its elements, and provides an example of applying the method to a two bus system to solve for the unknown voltage magnitude and angle at the second bus.
1. The document provides instructions to solve problems related to digital waveguide oscillators, digital lattice filters, and other discrete-time linear systems. Students are asked to write state space equations, find eigenvalues, compute responses, and represent systems using different forms such as state space and block diagrams. MATLAB code is provided to help with computations.
2. Students must analyze cascaded and parallel systems, check controllability and observability, and represent pulse transfer functions using state space, direct form, cascade form, and other block diagram representations. They are also asked to transform state space representations between different coordinate systems.
The document discusses equilibrium of particles and coplanar force systems. It has the following key points:
1) It introduces concepts of equilibrium, free body diagrams, and equations of equilibrium (scalar and vector forms) for solving 2D and 3D static equilibrium problems.
2) Examples are provided to demonstrate drawing free body diagrams and using the equations of equilibrium to solve for unknown forces in 2D and 3D systems involving cables, pulleys, springs, and other mechanics elements.
3) Procedures are outlined for setting up and solving static equilibrium problems involving both 2D coplanar and 3D non-coplanar force systems.
The document provides information about the format and marking scheme of the JEE (Advanced) exam from 2013, including:
- The exam has 3 parts (Physics, Chemistry, Mathematics) with 3 sections each: multiple choice with single correct answer, multiple choice with one or more correct answers, and questions with single-digit answers.
- Sections 1 and 3 award marks for correct answers and deduct marks for incorrect answers. Section 2 awards marks only for fully correct answers and deducts marks otherwise.
- An example question is provided for Section 1 of the Physics part of the exam.
The document discusses determining the angle between two lines and finding the point of intersection between two lines in 3D space. It provides the equations and process for finding the angle between two lines given their direction ratios. It also outlines the steps to find the point of intersection, which involves setting the coordinates of a point on each line equal to determine values for lambda and mu, and substituting those values back into one of the line equations. An example problem demonstrates finding the intersection point of two lines.
This document discusses statically indeterminate beams and methods for solving them. It begins by recapping free body diagrams, equilibrium, displacement compatibility, and force-displacement relations. It then introduces the procedure for solving statically indeterminate problems using the method of integration or method of superposition. Examples are provided to demonstrate applying these methods, including drawing free body diagrams, writing equilibrium equations, determining compatibility equations using boundary conditions, formulating moment equations, and integrating to find displacement equations. Key steps like determining constants of integration and unknown reactions using boundary conditions are shown. Finally, some remarks are made about accounting for shear and axial deformation in displacement calculations.
This document provides an overview of coplanar non-concurrent force systems and methods for analyzing them. It defines key terms like resultant, equilibrium, and equilibrant. Examples are provided to demonstrate determining resultants and support reactions for coplanar force systems, beams under different loading conditions, and plane trusses. Methods like Lami's theorem, free body diagrams, and the principles of equilibrium are used to solve for unknown forces. Truss analysis is also briefly discussed, noting trusses are articulated structures carrying loads at joints, with members in axial tension or compression.
Iit jam 2016 physics solutions BY TrajectoryeducationDev Singh
1. The electric field at a point (a, b, 0) due to an infinitely long wire with uniform line charge density λ is given by E=λ/(2πε0)(a/r2)ex+(b/r2)ey, where r2=a2+b2.
2. For a 1W point source emitting light uniformly in all directions, the Poynting vector at the point (1, 1, 0) is 1/(8π)ex+(y/e)ey W/cm2.
3. A charged particle starting from the origin with velocity 3/2ex+2ez m/s in a uniform magnetic field B=B
Deflection of structures using double integration method, moment area method, elastic load method, conjugate beam method, virtual work, castiglianois second theorem and method of consistent deformations
This module discusses coordinate proofs and properties of circles on the coordinate plane. It introduces coordinate proofs as an analytical method of proving geometric theorems by using the coordinates of points and algebraic relationships. Examples demonstrate proving properties of triangles and quadrilaterals analytically. The standard form of the equation of a circle is derived from the distance formula as (x - h)2 + (y - k)2 = r2, where (h, k) is the center and r is the radius. Finding the center, radius, and equation of circles in various forms are illustrated.
The document discusses the Newton-Raphson power flow method for solving power systems. Some key points:
- Newton-Raphson is commonly used for power flow analysis due to its fast convergence when initial guesses are close to the solution and large region of convergence. However, each iteration takes longer than Gauss-Seidel and it is more complicated to code.
- It uses Newton's method to determine the voltage magnitude and angle at each bus that satisfies the power balance equations. The power flow Jacobian matrix is calculated by differentiating the real and reactive power balance equations with respect to the voltage variables.
- A two-bus example demonstrates setting up and solving the power flow problem using Newton-Raphson
Determinants provide a scalar quantity associated with square matrices. There are several properties of determinants, including that the determinant of a matrix does not change if rows or columns are interchanged. The determinant can be expressed as the sum of the products of each element and its corresponding cofactor. Examples show how to evaluate determinants by expanding along rows or columns and applying properties such as identical rows resulting in a determinant of zero.
Determinants provide a scalar quantity associated with square matrices. There are several properties of determinants, including that the determinant of a matrix does not change if rows or columns are interchanged. The determinant can be expressed as the sum of the products of each element and its corresponding cofactor. Examples show how to evaluate determinants by expanding along rows or columns and applying properties such as identical rows resulting in a determinant of zero.
This document contains instructions for 12 math problems involving solving quadratic equations through various methods like factorization, using the quadratic formula, completing the square, and solving simultaneous linear equations and inequalities. Learners are asked to solve quadratic equations, determine if expressions are quadratic, factorize expressions, find the solution set of inequalities, and solve absolute value equations.
This document provides an overview of statics concepts including:
- Forces on particles in 2D and 3D space including addition and resolution of forces
- Equilibrium of particles and rigid bodies using free body diagrams
- Moments of forces about points and axes
- Force couples and equivalent force systems
- Example problems are provided to demonstrate applying concepts to determine tensions, components of forces, moments, and equivalent single forces.
1. The document discusses concepts related to force system resultants including cross products, moments of forces, and principles of moments.
2. It provides definitions and formulas for calculating the cross product of two vectors, the moment of a force about a point, and the resultant moment of a system of forces.
3. Examples are given to demonstrate calculating moments of forces using vector and scalar methods for different axis orientations.
This document outlines key concepts in 2D and 3D force systems. It begins by defining forces and force components in rectangular coordinate systems. It discusses concepts like concentrated vs distributed forces, and contact vs body forces. It also covers moments, couples, and resultants of force systems. Several example problems are provided to demonstrate calculating forces, moments, and resultants for 2D systems.
GraphSummit Singapore | The Art of the Possible with Graph - Q2 2024Neo4j
Neha Bajwa, Vice President of Product Marketing, Neo4j
Join us as we explore breakthrough innovations enabled by interconnected data and AI. Discover firsthand how organizations use relationships in data to uncover contextual insights and solve our most pressing challenges – from optimizing supply chains, detecting fraud, and improving customer experiences to accelerating drug discoveries.
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End-to-end overview of CI/CD pipeline with Azure devops
Speaker:
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Throughout the session, participants will discover how this synergy empowers testers to automate repetitive tasks, enhance testing accuracy, and expedite the software testing life cycle. Topics covered include the seamless integration process, practical use cases, and the benefits of harnessing AI-driven automation for UiPath testing initiatives. By attending this webinar, testers, and automation professionals can gain valuable insights into harnessing the power of AI to optimize their test automation workflows within the UiPath ecosystem, ultimately driving efficiency and quality in software development processes.
What will you get from this session?
1. Insights into integrating generative AI.
2. Understanding how this integration enhances test automation within the UiPath platform
3. Practical demonstrations
4. Exploration of real-world use cases illustrating the benefits of AI-driven test automation for UiPath
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Test Automation with generative AI and Open AI.
UiPath integration with generative AI
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1. FALCUTY OF APPLIED SCIENCE
ENGINEERING MECHANICS (AS1003)
HOMEWORK SUBMISSION
Group: CC01
Part: 1. Statics
Student’s fullname: Tran Quoc Thai
Stundent’s ID: 2153795
Semester: HK213
Lecturer: Assoc. Prof. Dr. Tich Thien TRUONG
Submission date: Sunday, July 17th, 2022
2. Problem 1:
Given a structure with supports and it is subjected a load as shown in figure 1. Given
M =5(KN.m), q = 10(KN/m), P = 9(KN), a = 0.5(m), α = 60°.
a) Prove that the structure is always in equilibrium under any applied loads.
b) Determine all support reactions at point D, B and reactions within AB bar.
(Assume that the weights of bodies are negligible)
3. Solution:
a)To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is always in equilibrium state under any
applied loads because
b)
1. Consider the equilibrium state for the bar DCB
Release two supports at two positions D and B.
Equilibrium equations:
2. Consider the equilibrium state for the bar AB
Release two supports at two positions A and B
3
1
3. 3.2 (2 2 2) 0
s
j
j
dof n R
1 2 .
Q a q
1
1
0(1)
0(2)
( ) . .2 0(3)
j D B
j D B
J B
F x H H
F y V Q P V
M F M P a Q a V
0
dof
4. '
'
' '
0(4)
0(5)
2 2 3
( ) . . 0(6)
3 3
j A B
j A B
J B B
F x H H
F y V V
M F V a H a
1
'
1
'
'
'
(3) . .2 10.5( ) 0
(5) 10.5( ) 0
(2) 9.5( ) 0
2
.
7 3
3
(6) 6.0622( ) 0
2
2 3
3
(4) 6.0622( ) 0
(1) 6.0622( ) 0
B
B B A
D B
B
B B
A B
D B
V M P a Q a KN
V V V KN
V Q P V KN
V a
H H KN
a
H H KN
H H KN
Equilibrium equations:
Solve the equilibrium equations:
5. Problem 2:
Given a structure with supports and there is an applied load on it shown in figure 2.
Given q, L, M=qL2. The weights of all bodies in the system and the frictions are
negligible.
a) Is the system always in equilibrium under any applied loads? Give the answer in
detail.
b) Determine all support reactions at A, C and E in term of q and L.
6. Solution:
a) To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is always in equilibrium state under any
applied loads because
b)
1. Consider the equilibrium state for the frame ABC
Release two supports at two positions A and C
Equilibrium equations:
2. Consider the equilibrium state for the bar CDE
Release two supports at two positions C and E
3
1
3. 3.2 (2 2 2) 0
s
j
j
dof n R
1
1
0(1)
0(2)
( ) . . . 0(3)
2
j A C
j A C
j C C
F x H H Q
F y V V
l
M F Q H l V l
0
dof
7. '
'
0(4)
0(5)
( ) . . 0(6)
j C E
J C E
j E E
F x H H
F y V V
M F M V l H l
*
'
'
1
(3) (6) 0
(5) 0( . )
(4) 0
(2) 0
(1) 2 0
C
E
C C E
C C A
A
V ql
V ql W D
H H H
V V V ql
H Q ql
Equilibrium equations:
Solve the equilibrium equations:
*(W.D): wrong direction
8. Problem 3:
Given a system with supports and it is subjected a linear load as shown in figure 3.
Given q, L, M=qL2. The weights of all bodies in the system and the frictions are
negligible.
a) Is the system always in equilibrium under any applied loads? Give the answer in
detail.
b) Determine all support reactions at A, C and E in term of q and L.
9. Solution:
a) To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is always in equilibrium state under any
applied loads because
b)
1. Consider the equilibrium state for the frame ABC
Release two supports at two positions A and C
Equilibrium equations:
2. Consider the equilibrium state for the bar CD
Release two supports at two positions C and D
3
1
3. 3.2 (2 2 2) 0
s
j
j
dof n R
0
dof
1
1
0(1)
0(2)
( ) . . . 0(3)
2
j A C
j A C
j C C
F x H H Q
F y V V
l
M F M Q H l V l
10. '
'
' '
0(4)
0(5)
( ) . . 0(6)
j C D
J C D
j C C
F x H H
F y V V
M F V l H l
'
'
(3) (6) 0
(5) 0( . )
(6) 0( . )
(4) 0( . )
(2) 0
(1) 0
C C
D
C C
D
A
A
V V ql
V ql W D
H H ql W D
H qL W D
V ql
H qL
Equilibrium equations:
Solve the equilibrium equations:
*(W.D): wrong direction
11. Problem 4:
A system is established as figure 4 with AB = 2a = CD = 2CB, F = qa. The weights of
bodies and frictions are negligible.
a) Is that system always in equilibrium with any applied load? Why?
b) Determine the reactions at A and B according to each of the two following
values of M.
- M = (√2q𝑎2 ) / 2
- M = 2qa
12. Solution:
a) To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is not always in equilibrium state under
any applied loads because
b)
1. Consider the equilibrium state for the bar DBC
Release two supports at two positions B and C
• We have:
Equilibrium condition:
The bar DBC must contact the frame AB at position B or
NB > 0
That means:
3
1
3. 3.2 (2 2 0.5) 0.5
s
j
j
dof n R
2
( ) . . .sin 0(1)
2
(2)
j B
B
M F M N BC F DC
qa M
N
a
2
2
2
2
(2) 0
2 0
2 (3)
qa M
a
qa M
M qa
0
dof
13. Case 1: Condition (2) is satisfied, that
means the system is always in equilibrium state under any
applied loads.
Substitute in equation (2) we get
• Consider the equilibrium state for the bar AB
• Release two supports at two positions A and B
Equilibrium equations:
Solve the equilibrium equations:
Case 2: Condition (2) is not satisfied, that
means the system is not in equilibrium state.So
Then:
2
2
2
qa
M
2
2
2
qa
M
2
0
2
B
qa
N
'
'
1
'
1
sin 0(4)
0(5)
( ) . 2 . cos 0(6)
j A B
j A B
j A B
F x H N
F y V N cos Q
M F M Q a a N
2
1
(4) 0
2
5
(5) 0
2
(6) 3 0
A
A
A
H qa
V qa
M qa
2
2
M qa
2
(4) 0
(5) 2 0
(6) 2
A
A
A
H
V qa
M qa
0
B
N
14. Problem 5:
A system is established as figure 5 with M = ql2. The weights of bodies and frictions are
negligible.
a) Is that system always in equilibrium with any applied load? Why?
b) Illustrate the reactions at A, C and E as functions of q and l.
15. Solution:
a)To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is always in equilibrium state under any
applied loads because
b)
1. Consider the equilibrium state for the frame ABC
Release two supports at two positions A and C.
Equilibrium equations:
2. Consider the equilibrium state for the bar CD
Release two supports at two positions C and D
3
1
3. 3.2 (2 2 2) 0
s
j
j
dof n R
1
1
0(1)
0(2)
( ) . . . 0(3)
2
j A C
j A C
j C C
F x H Q H
F y V V
l
M F Q H l V l
0
dof
ql
16. '
'
' '
0(4)
0(5)
( ) . . 0(6)
j C E
j C E
j C C
F x H H
F y V V
M F M V l H l
'
'
(3) (6) 0
(5) 0( . )
(6) 0( . )
(4) 0( . )
(2) 0
(1) 0
C C
E
C C
E
A
A
V V ql
V ql W D
H H ql W D
H qL W D
V ql
H qL
Equilibrium equations:
Solve the equilibrium equations:
*(W.D): wrong direction
17. Problem 6:
A system is established as figure 6 with P = 2qa, M = q𝑎2
. The weights of bodies
and frictions are negligible.
a) Is that system always in equilibrium with any applied load? Why?
b) Illustrate the reactions at A, B and D as functions of q and a.
18. Solution:
a)To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is always in equilibrium state under any
applied loads because
b)
1. Consider the equilibrium state for the bar AB
Release two supports at two positions A and B.
Equilibrium equations:
2. Consider the equilibrium state for the frame BCD
Release two supports at two positions B and D
3
1
3. 3.2 (2 2 2) 0
s
j
j
dof n R
1 2 .
Q a q
0(1)
0(2)
( ) . . . 0(3)
j A B
j A B
J B B
F x H H
F y V P V
M F H a V a P a
0
dof
a
a
y
x
a
a
𝑎
2
19. '
'
' '
0(4)
0(5)
( ) . . . 0(6)
2
j B D
j B D
j B C
F x H H Q
F y V V
a
M F M V a H a Q
'
'
7
(3) (6) 0
4
7
(5) 0( . )
4
15
(3) 0
4
15
(2) 0
4
15
(1) 0
4
11
(4) 0
4
B B
D
B B
A
A
D
V V qa
V qa W D
H H qa
V qa
H qa
H qa
Equilibrium equations:
Solve the equilibrium equations:
*(W.D): wrong direction
20. Problem 7:
Given a structure including beams and trusses on which there are forces like the diagram (Figure 7).
Friction forces and weights of all bodies can be neglected. It is stipulated that the reactions are negative
corresponding to compressed bars. Given 𝐹1= 6√2 kN, 𝐹2 = 6 kN, 𝐹3 = 4 kN, a= 1 m.
1) Determine the degree of freedom of the structure. Is the structure always in equilibrium under any
applied loads?
2) Determine reactions at cantilever A and all reactions exerted within ED bar.
3) Determine all reactions acted within bar 1 and bar 2.
21. Problem 8:
Given a structure with their supports on which there are external forces
like figure 8. Neglect friction forces at point D. Given a= 0.6 m, b= 0.4 m,
AD=2BD= 2a, CD=CE=b, P= 600N, Q=2P, q=1000 N/m. Determine all
reactions at cantilever A in two cases:
1) M= 300 Nm
2) M= 600 Nm
22. Solution:
a) To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is not always in equilibrium state under
any applied loads because
b)
1. Consider the equilibrium state for the bar ECD
Release two supports at two positions E and D
Equilibrium equations:
Equilibrium condition:
The bar DBC must contact the frame AB at position B or
ND > 0
That means:
3
1
3. 3.2 (2 3 0.5) 0.5
s
j
j
dof n R
0
dof
1
1
.cos30 0(1)
sin30 0(2)
3
( ) . . .sin30.2 0(3)
2
j E D
j D
j D
F x H N
F y P Q N
M F M P b Q b N b
E
D
y
x
C
P
1
1
1
3
.
2
(3) 0
2.sin30
3
. 0
2
3
. 1200( . )(4)
2
P Q M
P Q M
M P Q N m
23. Case 1: Condition (4) is satisfied, that
means the system is always in equilibrium state under any
applied loads.
Substitute in equation (3) we get
• Consider the equilibrium state for the bar ADB
• Release two supports at two positions A and B
Equilibrium equations:
Solve the equilibrium equations:
Case 2: Condition (4) is satisfied, that
means the system is always in equilibrium state under any
applied loads.
Substitute in equation (3) we get
300( . )
M N m
300
M 900( )
D
N N
'
'
' '
sin30 .cos30 0(5)
cos30 .sin30 0(6)
( ) .3 sin30. 3 cos30. 0(7)
j A D
j A D
j A D D
F x H N Q
F y V N Q
M F M Q a N a N a
(5) 1489.23 0 .
(6) 1379.42 0
(7) 2160 0
A
A
A
H W D
V
M
600( . )
M N m
(5) 1339.23 0 .
(6) 1119.62 0
(7) 2160 0
A
A
A
H W D
V
M
600
M 600( )
D
N N
24. Problem 9:
Given a mechanical structure includes their supports on which there are
external forces like figure 9. Given q, a, P= 2qa and M= q𝑎2 and all friction
forces and weights of bodies are negligible. Determine all reactions at A.
C and E in terms of q and a.
25. Solution:
a) To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is always in equilibrium state under any
applied loads because
b)
1. Consider the equilibrium state for the frame ABC
Release two supports at two positions A and C
Equilibrium equations:
2. Consider the equilibrium state for the frame CDE
Release two supports at two positions C and E
3
1
3. 3.2 (2 2 2) 0
s
j
j
dof n R
0
dof
0(1)
0(2)
( ) . . . 0(3)
j A C
j A C
j C C
F x H H
F y V P V
M F H a P a V a
A
B
C
y
x
a
a
C
E
D
M
y
x
a
a
26. '
'
' '
0(4)
0(5)
( ) . . . 0(6)
2
j C E
j C E
j C C
F x H H
F y V V Q
a
M F M V a H a Q
'
'
1
(3) (6) 0
4
7
(2) 0( . )
4
7
(3) 0( . )
4
7
(1) 0( . )
4
7
(4) 0( . )
4
5
(5) 0( . )
4
C C
A
C C
A
E
E
V V qa
V qa W D
H H qa W D
H qa W D
H qa W D
V qa W D
Equilibrium equations:
Solve the equilibrium equations:
*(W.D): wrong direction
27. Problem 10:
A mechanical system is shown as in figure 10 with a = 0.6 m, b = 0.4 m, AB = 2a, P =
600 N, CB = BD = DE = b, q = 1000 N/m. Friction at B is negligible. Determine the
reactions at support A corresponding to each of the following conditions.
1) M = 500 Nm
2) M = 700 Nm
28. Solution:
a) To consider the equilibrium state of the structure, we
compute dof of the system.
This structure is not always in equilibrium state under
any applied loads because
b)
1. Consider the equilibrium state for the bar EDBC
Release two supports at two positions E and B
• We have:
Equilibrium condition: The bar EDBC must contact the bar
AB at position B or NB > 0
That means:
3
1
3. 3.2 (2 2 0.5) 0.5
s
j
j
dof n R
5
( ) . .2 . 0(1)
2
5
. .
2 (2)
2
j B
B
M F M P b N b Q b
P b Q b M
N
b
5
. .
2
(2) 0
2
5
. . 0
2
160(3)
P b Q b M
b
P b Q b M
M
0
dof
E D B C
x
y
P
M
b b
b
Q
5b/2
𝑁𝐵
𝑉𝐸
𝐻𝐵
29. Case 1: Condition (3) not is satisfied, that
means the system is not in equilibrium state under any
applied loads.
That means
• Consider the equilibrium state for the bar AB
• Release two supports at two positions A and B
Equilibrium equations:
Solve the equilibrium equations:
Case 2: Condition (3) is not satisfied, that
means the system is not in equilibrium state under any
applied loads.
That means
500( . )
M N m
0( )
B
N N
0(4)
0(5)
( ) 0(6)
j A
j A
j A
F x H
F y V
M F M
(4) 0
(5) 0
(6) 0
A
A
A
H
V
M
600( . )
M N m
(5) 0
(6) 0
(7) 0
A
A
A
H
V
M
0( )
D
N N
y
x
A
B
𝑁𝐵
′
30. Problem 11:
A mechanical system is shown as in figure 11 with R = 2r = 1 m; 𝛼 = 60°,
AB = 3m, P = 2 KN, Q = 1 KN, M = 1.5 KNm.
Determine the reactions at A and the tensile force at E. The friction at
external pin B is negligible