SlideShare une entreprise Scribd logo
1  sur  18
Télécharger pour lire hors ligne
Unit 1- Stress and Strain
Topics Covered
  Lecture -1 - Introduction, state of plane stress

  Lecture -2 - Principle Stresses and Strains

  Lecture -3 - Mohr's Stress Circle and Theory of
   Failure

  Lecture -4- 3-D stress and strain, Equilibrium
   equations and impact loading

  Lecture -5 - Generalized Hook's law and Castigliono's
3-D Stress and Strain
          stress vector σ that represents the force per
          unit area acting at a given location on the
          body's surface.
          In other words, a stress vector cannot be fully
            €
          described unless both the force and the
          surface where the force acts on has been
          specified.
                              ΔF dF
                   σ = lim       =
                        Δs−>0 Δs   ds



         €
3-D Stress and Strain

          Suppose an arbitrary slice is made across the
          solid shown in the above figure, leading to
          the free body diagram shown at left. Stress
          would appear on the exposed surface, similar
          in form to the external stress applied to the
          body's exterior surface. The stress at point P
          can be defined using the same above
          equation
3-D Stress and Strain
          Stresses acting on an plane, are typically
          decomposed into three mutually orthogonal
          components. One component is normal to
          the surface and represents direct stress. The
          other two components are tangential to the
          surface and represent shear stresses.


          Normal component = σxx ,σyy ,σzz


          Tangential component = xy ,σyx ,σxz ,σzx ,σyz ,σzy
                                σ
                       €


                      €
3-D Stress and Strain
                                        Since each point on the cube is under static
                                        equilibrium (no net force in the absense of
                                        any body forces), only nine stress
                                        components from three planes are needed to
                                        describe the stress state at a point P.
                                        These nine components can be organized
                                        into the matrix:

                                                     ⎡σ       σxy σxz ⎤
                                                         xx
                                                     ⎢                ⎥
                                                     ⎢σyx     σyy σyz ⎥
                                                     ⎢σ
                                                     ⎣ zx     σzy σzz ⎥
                                                                       ⎦
In this course we are also     where shear stresses across the diagonal are identical
denoting shear stresses as τ   as a result of static equilibrium (no net moment). This
                               grouping of the nine stress components is known as
                               the stress tensor (or stress matrix).

             €                        €
3-D Stress and Strain
           Shear stresses across the diagonal are
           identical as a result of static equilibrium (no
           net moment). The six shear stresses reduces
           to 3 shear stresses.
           This grouping of the six stress components is
           known as the stress tensor (or stress matrix).

        The off diagonal elements are equal i.e   σxy = σyx
                        ⎡σ       σxy σxz ⎤
                            xx
                        ⎢                ⎥
                        ⎢σxy     σyy σyz ⎥
                                    €
                        ⎢σ
                        ⎣ xz     σyz σzz ⎥
                                          ⎦



         €
Equilibrium equations
                            ∂σyy
                      σyy +      dy
                             ∂y                              X, Y – body force such as weight of the body
         Y                                     ∂σyx
                                         σyx +      dy
                                                ∂y
             σxy         Y
    €
                                                        ∂σxx
        dy σ                                      σxx +      dx
             xx              €       X                   ∂x
€
                                             σxy +
                                                   ∂σxy
                                                    ∂x
                                                        dx                                   ∑F     x   =0
                  σyx            σyy€
€                                             X
                                                       ⎛      ∂σxx ⎞
                             dx                        ⎜σxx +     dx ⎟(dy × 1) − σxx ( dy × 1) +
                                 €                     ⎝       ∂x    ⎠
    €             €                                    ⎛      ∂σyx ⎞ €
                                                       ⎜σyx +     dy ⎟( dx × 1) − σyx ( dx × 1) + X ( dxdy × 1) = 0
                                                       ⎝       ∂y    ⎠



                                         €
Equilibrium equations
                            ∂σyy
                      σyy +      dy
                             ∂y
                                               ∂σyx             For 2 dimension
          y                              σyx +      dy
                                                ∂y
              σxy
    €
                         Y
                                                                   ∂σ xx ∂σ xy
        dy σ                                    σxx +
                                                      ∂σxx
                                                           dx           +      +X =0
             xx              €       X                 ∂x           ∂x    ∂y
€                                                ∂σxy
                                           σxy +
                                                  ∂x
                                                      dx           ∂σ yx ∂σ yy
                  σyx            σyy€                                   +      +Y = 0
€                                           x                       ∂x    ∂y
                             dx
                                 €
    €             €
                                                X, Y – body force such as weight of the body
                                                  €
Equilibrium equations
     For 3 dimension

   ∂σ xx ∂σ xy ∂σ xz
        +     +      +X =0
    ∂x    ∂y    ∂z
   ∂σ yx ∂σ yy ∂σ yz
        +     +      +Y = 0
    ∂x    ∂y    ∂z
   ∂σ zx ∂σ zy ∂σ zz
        +     +      +Z =0
    ∂x    ∂y    ∂z
Impact Load
  Definitions
     Resilience – Total strain energy stored in the system.
     Proof resilience – Maximum strain energy stored in a
      body is known as proof resilience. Strain energy in the
      body will be maximum when the body is stressed upto
      elastic limit
     Modulus of resilience- Proof resilience of a material
      per unit volume.
                                  Pr oof _ resilience
      Modulus of resilience =
                                Volume _ of _ the _ body



                   €
Impact Load
  Strain energy when load is applied gradually.

                                                              M
                             2
  Energy stored in a body=
                             σV
                                   Load
                             2E           P

                          σ 2 AL                              N
                        =
                           2E                 O   Extension
             €                                      x



         €
Impact Load
              Strain energy when load is applied suddenly.

                                                                             M
                                            2
                Energy stored in a body=
                                           σ AL
                                                  Load
                                            2E           P

                σ 2 AL           σ
                       =P×x=P× ×L                                            N
                 2E              E                           O   Extension
                       €       P                                   x
                         σ =2×
                               A
    derivation in book - R.K Bansal
€
Impact Load
  PROBLEM- A steel rod is 2m long and 50mm in
   diameter. An axial pull of 100 kN is suddenly
   applied to the rod. Calculate the instantaneous stress
   induced and also the instantaneous elongation
   produced in the rod. Take E=200GN/mm2
Impact Load
      Strain energy when load is applied with impact.
       Energy of impact = Potential energy of the falling load
                              σ 2 AL
       Energy of impact =
                               2E
      Potential energy of the falling load = P   ( h + δL )

              €
              P ⎛    €2AEh ⎞
           σ = ⎜1+ 1+      ⎟
              A ⎝      PL ⎠



€
Impact Load
                             PROBLEM- A vertical compound tie
                                 member fixed rigidly at its upper end
            20 mm                consists of a steel rod 2.5 m long and
2.5 m                   P=10kN   30mm external diameter. The rod and
        1           2
                                 the tube are fixed together at the ends.
                         3 mm    The compound member is then
                                 suddenly loaded in tension by a weight
            21 mm                of 10 kN falling through a height of 3
                                 mm on to a flange fixed to its lower
            30 mm
                                 end. Calculate the maximum stresses
                                 in steel and brass. Assume Es=2x105
                                 N/mm2 and Eb=1.0x105 N/mm2
Impact Load
  Strain energy in shear loading.

                          τ 2 AL
   Strain energy stored =
                           2C                                     P
                                             D       D1       C       C1


            €

                                         h

                                                 φ                φ
                                             A            l   B


                                     €                €
Impact Load
  PROBLEM- The shear stress in a material at a price
   is given as 50N/mm2. Determine the local strain
   energy per unit volume stored in the material due to
   shear stress. Take C=8x104 N/mm2

Contenu connexe

Tendances

03 tensors
03 tensors03 tensors
03 tensors
Tino Lc
 

Tendances (20)

Simple stresses and strain
Simple stresses and strainSimple stresses and strain
Simple stresses and strain
 
03 tensors
03 tensors03 tensors
03 tensors
 
Lecture 1 stresses and strains
Lecture 1 stresses and strainsLecture 1 stresses and strains
Lecture 1 stresses and strains
 
Finite Element Analysis - UNIT-2
Finite Element Analysis - UNIT-2Finite Element Analysis - UNIT-2
Finite Element Analysis - UNIT-2
 
theory of elasticity
theory of elasticitytheory of elasticity
theory of elasticity
 
Theories of failure
Theories of failureTheories of failure
Theories of failure
 
Chapter 1 stress and strain
Chapter 1   stress and strainChapter 1   stress and strain
Chapter 1 stress and strain
 
Engineering Mechanics
Engineering MechanicsEngineering Mechanics
Engineering Mechanics
 
A presentation on shear stress (10.01.03.139)
A presentation on shear stress (10.01.03.139)A presentation on shear stress (10.01.03.139)
A presentation on shear stress (10.01.03.139)
 
UNIT-I-Theories of failures-19072016.pptx
UNIT-I-Theories of failures-19072016.pptxUNIT-I-Theories of failures-19072016.pptx
UNIT-I-Theories of failures-19072016.pptx
 
Theories of failure
Theories of failureTheories of failure
Theories of failure
 
Contact stresses
Contact stressesContact stresses
Contact stresses
 
Energy methods
Energy methodsEnergy methods
Energy methods
 
Isoparametric bilinear quadrilateral element _ ppt presentation
Isoparametric bilinear quadrilateral element _ ppt presentationIsoparametric bilinear quadrilateral element _ ppt presentation
Isoparametric bilinear quadrilateral element _ ppt presentation
 
Chapter 3: Generalized Hooke's Law, Pressure Vessels, and Thick-Walled Cylinders
Chapter 3: Generalized Hooke's Law, Pressure Vessels, and Thick-Walled CylindersChapter 3: Generalized Hooke's Law, Pressure Vessels, and Thick-Walled Cylinders
Chapter 3: Generalized Hooke's Law, Pressure Vessels, and Thick-Walled Cylinders
 
Unsymmetrical bending.ppt
Unsymmetrical bending.pptUnsymmetrical bending.ppt
Unsymmetrical bending.ppt
 
6 Machine design theories of failure
6 Machine design theories of failure6 Machine design theories of failure
6 Machine design theories of failure
 
FEM: Introduction and Weighted Residual Methods
FEM: Introduction and Weighted Residual MethodsFEM: Introduction and Weighted Residual Methods
FEM: Introduction and Weighted Residual Methods
 
4 pure bending
4 pure bending4 pure bending
4 pure bending
 
Strength of materials
Strength of materialsStrength of materials
Strength of materials
 

Similaire à Lecture 4 3 d stress tensor and equilibrium equations

Kinematics of a fluid element
Kinematics of a fluid elementKinematics of a fluid element
Kinematics of a fluid element
Mohamed Yaser
 
Kinematics of a fluid element
Kinematics of a fluid elementKinematics of a fluid element
Kinematics of a fluid element
Mohamed Yaser
 
Basic differential equations in fluid mechanics
Basic differential equations in fluid mechanicsBasic differential equations in fluid mechanics
Basic differential equations in fluid mechanics
Tarun Gehlot
 
Emat 213 study guide
Emat 213 study guideEmat 213 study guide
Emat 213 study guide
akabaka12
 
Bai giang ham so kha vi va vi phan cua ham nhieu bien
Bai giang ham so kha vi va vi phan cua ham nhieu bienBai giang ham so kha vi va vi phan cua ham nhieu bien
Bai giang ham so kha vi va vi phan cua ham nhieu bien
Nhan Nguyen
 
Cs229 cvxopt
Cs229 cvxoptCs229 cvxopt
Cs229 cvxopt
cerezaso
 

Similaire à Lecture 4 3 d stress tensor and equilibrium equations (20)

Beam theory
Beam theoryBeam theory
Beam theory
 
Theory of elasticity and plasticity (Equations sheet part 01) Att 8676
Theory of elasticity and plasticity (Equations sheet part 01) Att 8676Theory of elasticity and plasticity (Equations sheet part 01) Att 8676
Theory of elasticity and plasticity (Equations sheet part 01) Att 8676
 
Hw2 s
Hw2 sHw2 s
Hw2 s
 
UDA 5 - P.pdf
UDA 5 - P.pdfUDA 5 - P.pdf
UDA 5 - P.pdf
 
Kinematics of a fluid element
Kinematics of a fluid elementKinematics of a fluid element
Kinematics of a fluid element
 
Kinematics of a fluid element
Kinematics of a fluid elementKinematics of a fluid element
Kinematics of a fluid element
 
Chapter 4
Chapter 4Chapter 4
Chapter 4
 
iTute Notes MM
iTute Notes MMiTute Notes MM
iTute Notes MM
 
Universal algebra (1)
Universal algebra (1)Universal algebra (1)
Universal algebra (1)
 
集合知プログラミングゼミ第1回
集合知プログラミングゼミ第1回集合知プログラミングゼミ第1回
集合知プログラミングゼミ第1回
 
Basic differential equations in fluid mechanics
Basic differential equations in fluid mechanicsBasic differential equations in fluid mechanics
Basic differential equations in fluid mechanics
 
Double integration
Double integrationDouble integration
Double integration
 
Emat 213 study guide
Emat 213 study guideEmat 213 study guide
Emat 213 study guide
 
Cross product
Cross productCross product
Cross product
 
Stress5_ht08.pdf
Stress5_ht08.pdfStress5_ht08.pdf
Stress5_ht08.pdf
 
Tensor 1
Tensor  1Tensor  1
Tensor 1
 
Bai giang ham so kha vi va vi phan cua ham nhieu bien
Bai giang ham so kha vi va vi phan cua ham nhieu bienBai giang ham so kha vi va vi phan cua ham nhieu bien
Bai giang ham so kha vi va vi phan cua ham nhieu bien
 
AlgoPerm2012 - 03 Olivier Hudry
AlgoPerm2012 - 03 Olivier HudryAlgoPerm2012 - 03 Olivier Hudry
AlgoPerm2012 - 03 Olivier Hudry
 
Cs229 cvxopt
Cs229 cvxoptCs229 cvxopt
Cs229 cvxopt
 
Moh'r circle2
Moh'r circle2Moh'r circle2
Moh'r circle2
 

Plus de Deepak Agarwal

MS_thesis_presentation
MS_thesis_presentationMS_thesis_presentation
MS_thesis_presentation
Deepak Agarwal
 
Lecture 13 torsion in solid and hollow shafts 1
Lecture 13 torsion in solid and hollow shafts 1Lecture 13 torsion in solid and hollow shafts 1
Lecture 13 torsion in solid and hollow shafts 1
Deepak Agarwal
 
Lecture 12 deflection in beams
Lecture 12 deflection in beamsLecture 12 deflection in beams
Lecture 12 deflection in beams
Deepak Agarwal
 
Lecture 11 shear stresses in beams
Lecture 11 shear stresses in beamsLecture 11 shear stresses in beams
Lecture 11 shear stresses in beams
Deepak Agarwal
 
Lecture 10 bending stresses in beams
Lecture 10 bending stresses in beamsLecture 10 bending stresses in beams
Lecture 10 bending stresses in beams
Deepak Agarwal
 
Lecture 9 shear force and bending moment in beams
Lecture 9 shear force and bending moment in beamsLecture 9 shear force and bending moment in beams
Lecture 9 shear force and bending moment in beams
Deepak Agarwal
 
Lecture 5 castigliono's theorem
Lecture 5 castigliono's theoremLecture 5 castigliono's theorem
Lecture 5 castigliono's theorem
Deepak Agarwal
 
Lecture 3 mohr’s circle and theory of failure
Lecture 3 mohr’s circle and theory of failure Lecture 3 mohr’s circle and theory of failure
Lecture 3 mohr’s circle and theory of failure
Deepak Agarwal
 

Plus de Deepak Agarwal (8)

MS_thesis_presentation
MS_thesis_presentationMS_thesis_presentation
MS_thesis_presentation
 
Lecture 13 torsion in solid and hollow shafts 1
Lecture 13 torsion in solid and hollow shafts 1Lecture 13 torsion in solid and hollow shafts 1
Lecture 13 torsion in solid and hollow shafts 1
 
Lecture 12 deflection in beams
Lecture 12 deflection in beamsLecture 12 deflection in beams
Lecture 12 deflection in beams
 
Lecture 11 shear stresses in beams
Lecture 11 shear stresses in beamsLecture 11 shear stresses in beams
Lecture 11 shear stresses in beams
 
Lecture 10 bending stresses in beams
Lecture 10 bending stresses in beamsLecture 10 bending stresses in beams
Lecture 10 bending stresses in beams
 
Lecture 9 shear force and bending moment in beams
Lecture 9 shear force and bending moment in beamsLecture 9 shear force and bending moment in beams
Lecture 9 shear force and bending moment in beams
 
Lecture 5 castigliono's theorem
Lecture 5 castigliono's theoremLecture 5 castigliono's theorem
Lecture 5 castigliono's theorem
 
Lecture 3 mohr’s circle and theory of failure
Lecture 3 mohr’s circle and theory of failure Lecture 3 mohr’s circle and theory of failure
Lecture 3 mohr’s circle and theory of failure
 

Dernier

Russian Call Girls In Pune 👉 Just CALL ME: 9352988975 ✅❤️💯low cost unlimited ...
Russian Call Girls In Pune 👉 Just CALL ME: 9352988975 ✅❤️💯low cost unlimited ...Russian Call Girls In Pune 👉 Just CALL ME: 9352988975 ✅❤️💯low cost unlimited ...
Russian Call Girls In Pune 👉 Just CALL ME: 9352988975 ✅❤️💯low cost unlimited ...
chanderprakash5506
 
👉 Chennai Sexy Aunty’s WhatsApp Number 👉📞 7427069034 👉📞 Just📲 Call Ruhi Colle...
👉 Chennai Sexy Aunty’s WhatsApp Number 👉📞 7427069034 👉📞 Just📲 Call Ruhi Colle...👉 Chennai Sexy Aunty’s WhatsApp Number 👉📞 7427069034 👉📞 Just📲 Call Ruhi Colle...
👉 Chennai Sexy Aunty’s WhatsApp Number 👉📞 7427069034 👉📞 Just📲 Call Ruhi Colle...
rajnisinghkjn
 
Difference Between Skeletal Smooth and Cardiac Muscles
Difference Between Skeletal Smooth and Cardiac MusclesDifference Between Skeletal Smooth and Cardiac Muscles
Difference Between Skeletal Smooth and Cardiac Muscles
MedicoseAcademics
 
Call Girl in Chennai | Whatsapp No 📞 7427069034 📞 VIP Escorts Service Availab...
Call Girl in Chennai | Whatsapp No 📞 7427069034 📞 VIP Escorts Service Availab...Call Girl in Chennai | Whatsapp No 📞 7427069034 📞 VIP Escorts Service Availab...
Call Girl in Chennai | Whatsapp No 📞 7427069034 📞 VIP Escorts Service Availab...
amritaverma53
 
Cara Menggugurkan Kandungan Dengan Cepat Selesai Dalam 24 Jam Secara Alami Bu...
Cara Menggugurkan Kandungan Dengan Cepat Selesai Dalam 24 Jam Secara Alami Bu...Cara Menggugurkan Kandungan Dengan Cepat Selesai Dalam 24 Jam Secara Alami Bu...
Cara Menggugurkan Kandungan Dengan Cepat Selesai Dalam 24 Jam Secara Alami Bu...
Cara Menggugurkan Kandungan 087776558899
 

Dernier (20)

💞 Safe And Secure Call Girls Coimbatore🧿 6378878445 🧿 High Class Coimbatore C...
💞 Safe And Secure Call Girls Coimbatore🧿 6378878445 🧿 High Class Coimbatore C...💞 Safe And Secure Call Girls Coimbatore🧿 6378878445 🧿 High Class Coimbatore C...
💞 Safe And Secure Call Girls Coimbatore🧿 6378878445 🧿 High Class Coimbatore C...
 
Russian Call Girls In Pune 👉 Just CALL ME: 9352988975 ✅❤️💯low cost unlimited ...
Russian Call Girls In Pune 👉 Just CALL ME: 9352988975 ✅❤️💯low cost unlimited ...Russian Call Girls In Pune 👉 Just CALL ME: 9352988975 ✅❤️💯low cost unlimited ...
Russian Call Girls In Pune 👉 Just CALL ME: 9352988975 ✅❤️💯low cost unlimited ...
 
Call Girls Kathua Just Call 8250077686 Top Class Call Girl Service Available
Call Girls Kathua Just Call 8250077686 Top Class Call Girl Service AvailableCall Girls Kathua Just Call 8250077686 Top Class Call Girl Service Available
Call Girls Kathua Just Call 8250077686 Top Class Call Girl Service Available
 
Circulatory Shock, types and stages, compensatory mechanisms
Circulatory Shock, types and stages, compensatory mechanismsCirculatory Shock, types and stages, compensatory mechanisms
Circulatory Shock, types and stages, compensatory mechanisms
 
Race Course Road } Book Call Girls in Bangalore | Whatsapp No 6378878445 VIP ...
Race Course Road } Book Call Girls in Bangalore | Whatsapp No 6378878445 VIP ...Race Course Road } Book Call Girls in Bangalore | Whatsapp No 6378878445 VIP ...
Race Course Road } Book Call Girls in Bangalore | Whatsapp No 6378878445 VIP ...
 
Call Girls in Lucknow Just Call 👉👉8630512678 Top Class Call Girl Service Avai...
Call Girls in Lucknow Just Call 👉👉8630512678 Top Class Call Girl Service Avai...Call Girls in Lucknow Just Call 👉👉8630512678 Top Class Call Girl Service Avai...
Call Girls in Lucknow Just Call 👉👉8630512678 Top Class Call Girl Service Avai...
 
👉 Chennai Sexy Aunty’s WhatsApp Number 👉📞 7427069034 👉📞 Just📲 Call Ruhi Colle...
👉 Chennai Sexy Aunty’s WhatsApp Number 👉📞 7427069034 👉📞 Just📲 Call Ruhi Colle...👉 Chennai Sexy Aunty’s WhatsApp Number 👉📞 7427069034 👉📞 Just📲 Call Ruhi Colle...
👉 Chennai Sexy Aunty’s WhatsApp Number 👉📞 7427069034 👉📞 Just📲 Call Ruhi Colle...
 
Bhawanipatna Call Girls 📞9332606886 Call Girls in Bhawanipatna Escorts servic...
Bhawanipatna Call Girls 📞9332606886 Call Girls in Bhawanipatna Escorts servic...Bhawanipatna Call Girls 📞9332606886 Call Girls in Bhawanipatna Escorts servic...
Bhawanipatna Call Girls 📞9332606886 Call Girls in Bhawanipatna Escorts servic...
 
Chennai ❣️ Call Girl 6378878445 Call Girls in Chennai Escort service book now
Chennai ❣️ Call Girl 6378878445 Call Girls in Chennai Escort service book nowChennai ❣️ Call Girl 6378878445 Call Girls in Chennai Escort service book now
Chennai ❣️ Call Girl 6378878445 Call Girls in Chennai Escort service book now
 
Lucknow Call Girls Just Call 👉👉8630512678 Top Class Call Girl Service Available
Lucknow Call Girls Just Call 👉👉8630512678 Top Class Call Girl Service AvailableLucknow Call Girls Just Call 👉👉8630512678 Top Class Call Girl Service Available
Lucknow Call Girls Just Call 👉👉8630512678 Top Class Call Girl Service Available
 
Call Girls Mussoorie Just Call 8854095900 Top Class Call Girl Service Available
Call Girls Mussoorie Just Call 8854095900 Top Class Call Girl Service AvailableCall Girls Mussoorie Just Call 8854095900 Top Class Call Girl Service Available
Call Girls Mussoorie Just Call 8854095900 Top Class Call Girl Service Available
 
Difference Between Skeletal Smooth and Cardiac Muscles
Difference Between Skeletal Smooth and Cardiac MusclesDifference Between Skeletal Smooth and Cardiac Muscles
Difference Between Skeletal Smooth and Cardiac Muscles
 
Cardiac Output, Venous Return, and Their Regulation
Cardiac Output, Venous Return, and Their RegulationCardiac Output, Venous Return, and Their Regulation
Cardiac Output, Venous Return, and Their Regulation
 
Call Girls Wayanad Just Call 8250077686 Top Class Call Girl Service Available
Call Girls Wayanad Just Call 8250077686 Top Class Call Girl Service AvailableCall Girls Wayanad Just Call 8250077686 Top Class Call Girl Service Available
Call Girls Wayanad Just Call 8250077686 Top Class Call Girl Service Available
 
Call Girl in Chennai | Whatsapp No 📞 7427069034 📞 VIP Escorts Service Availab...
Call Girl in Chennai | Whatsapp No 📞 7427069034 📞 VIP Escorts Service Availab...Call Girl in Chennai | Whatsapp No 📞 7427069034 📞 VIP Escorts Service Availab...
Call Girl in Chennai | Whatsapp No 📞 7427069034 📞 VIP Escorts Service Availab...
 
Call girls Service Phullen / 9332606886 Genuine Call girls with real Photos a...
Call girls Service Phullen / 9332606886 Genuine Call girls with real Photos a...Call girls Service Phullen / 9332606886 Genuine Call girls with real Photos a...
Call girls Service Phullen / 9332606886 Genuine Call girls with real Photos a...
 
ANATOMY AND PHYSIOLOGY OF REPRODUCTIVE SYSTEM.pptx
ANATOMY AND PHYSIOLOGY OF REPRODUCTIVE SYSTEM.pptxANATOMY AND PHYSIOLOGY OF REPRODUCTIVE SYSTEM.pptx
ANATOMY AND PHYSIOLOGY OF REPRODUCTIVE SYSTEM.pptx
 
Cara Menggugurkan Kandungan Dengan Cepat Selesai Dalam 24 Jam Secara Alami Bu...
Cara Menggugurkan Kandungan Dengan Cepat Selesai Dalam 24 Jam Secara Alami Bu...Cara Menggugurkan Kandungan Dengan Cepat Selesai Dalam 24 Jam Secara Alami Bu...
Cara Menggugurkan Kandungan Dengan Cepat Selesai Dalam 24 Jam Secara Alami Bu...
 
Call Girls in Lucknow Just Call 👉👉 8875999948 Top Class Call Girl Service Ava...
Call Girls in Lucknow Just Call 👉👉 8875999948 Top Class Call Girl Service Ava...Call Girls in Lucknow Just Call 👉👉 8875999948 Top Class Call Girl Service Ava...
Call Girls in Lucknow Just Call 👉👉 8875999948 Top Class Call Girl Service Ava...
 
ANATOMY AND PHYSIOLOGY OF RESPIRATORY SYSTEM.pptx
ANATOMY AND PHYSIOLOGY OF RESPIRATORY SYSTEM.pptxANATOMY AND PHYSIOLOGY OF RESPIRATORY SYSTEM.pptx
ANATOMY AND PHYSIOLOGY OF RESPIRATORY SYSTEM.pptx
 

Lecture 4 3 d stress tensor and equilibrium equations

  • 1.
  • 2. Unit 1- Stress and Strain Topics Covered   Lecture -1 - Introduction, state of plane stress   Lecture -2 - Principle Stresses and Strains   Lecture -3 - Mohr's Stress Circle and Theory of Failure   Lecture -4- 3-D stress and strain, Equilibrium equations and impact loading   Lecture -5 - Generalized Hook's law and Castigliono's
  • 3. 3-D Stress and Strain stress vector σ that represents the force per unit area acting at a given location on the body's surface. In other words, a stress vector cannot be fully € described unless both the force and the surface where the force acts on has been specified. ΔF dF σ = lim = Δs−>0 Δs ds €
  • 4. 3-D Stress and Strain Suppose an arbitrary slice is made across the solid shown in the above figure, leading to the free body diagram shown at left. Stress would appear on the exposed surface, similar in form to the external stress applied to the body's exterior surface. The stress at point P can be defined using the same above equation
  • 5. 3-D Stress and Strain Stresses acting on an plane, are typically decomposed into three mutually orthogonal components. One component is normal to the surface and represents direct stress. The other two components are tangential to the surface and represent shear stresses. Normal component = σxx ,σyy ,σzz Tangential component = xy ,σyx ,σxz ,σzx ,σyz ,σzy σ € €
  • 6. 3-D Stress and Strain Since each point on the cube is under static equilibrium (no net force in the absense of any body forces), only nine stress components from three planes are needed to describe the stress state at a point P. These nine components can be organized into the matrix: ⎡σ σxy σxz ⎤ xx ⎢ ⎥ ⎢σyx σyy σyz ⎥ ⎢σ ⎣ zx σzy σzz ⎥ ⎦ In this course we are also where shear stresses across the diagonal are identical denoting shear stresses as τ as a result of static equilibrium (no net moment). This grouping of the nine stress components is known as the stress tensor (or stress matrix). € €
  • 7. 3-D Stress and Strain Shear stresses across the diagonal are identical as a result of static equilibrium (no net moment). The six shear stresses reduces to 3 shear stresses. This grouping of the six stress components is known as the stress tensor (or stress matrix). The off diagonal elements are equal i.e σxy = σyx ⎡σ σxy σxz ⎤ xx ⎢ ⎥ ⎢σxy σyy σyz ⎥ € ⎢σ ⎣ xz σyz σzz ⎥ ⎦ €
  • 8. Equilibrium equations ∂σyy σyy + dy ∂y X, Y – body force such as weight of the body Y ∂σyx σyx + dy ∂y σxy Y € ∂σxx dy σ σxx + dx xx € X ∂x € σxy + ∂σxy ∂x dx ∑F x =0 σyx σyy€ € X ⎛ ∂σxx ⎞ dx ⎜σxx + dx ⎟(dy × 1) − σxx ( dy × 1) + € ⎝ ∂x ⎠ € € ⎛ ∂σyx ⎞ € ⎜σyx + dy ⎟( dx × 1) − σyx ( dx × 1) + X ( dxdy × 1) = 0 ⎝ ∂y ⎠ €
  • 9. Equilibrium equations ∂σyy σyy + dy ∂y ∂σyx For 2 dimension y σyx + dy ∂y σxy € Y ∂σ xx ∂σ xy dy σ σxx + ∂σxx dx + +X =0 xx € X ∂x ∂x ∂y € ∂σxy σxy + ∂x dx ∂σ yx ∂σ yy σyx σyy€ + +Y = 0 € x ∂x ∂y dx € € € X, Y – body force such as weight of the body €
  • 10. Equilibrium equations For 3 dimension ∂σ xx ∂σ xy ∂σ xz + + +X =0 ∂x ∂y ∂z ∂σ yx ∂σ yy ∂σ yz + + +Y = 0 ∂x ∂y ∂z ∂σ zx ∂σ zy ∂σ zz + + +Z =0 ∂x ∂y ∂z
  • 11. Impact Load   Definitions   Resilience – Total strain energy stored in the system.   Proof resilience – Maximum strain energy stored in a body is known as proof resilience. Strain energy in the body will be maximum when the body is stressed upto elastic limit   Modulus of resilience- Proof resilience of a material per unit volume. Pr oof _ resilience Modulus of resilience = Volume _ of _ the _ body €
  • 12. Impact Load   Strain energy when load is applied gradually. M 2 Energy stored in a body= σV Load 2E P σ 2 AL N = 2E O Extension € x €
  • 13. Impact Load   Strain energy when load is applied suddenly. M 2 Energy stored in a body= σ AL Load 2E P σ 2 AL σ =P×x=P× ×L N 2E E O Extension € P x σ =2× A derivation in book - R.K Bansal €
  • 14. Impact Load   PROBLEM- A steel rod is 2m long and 50mm in diameter. An axial pull of 100 kN is suddenly applied to the rod. Calculate the instantaneous stress induced and also the instantaneous elongation produced in the rod. Take E=200GN/mm2
  • 15. Impact Load   Strain energy when load is applied with impact. Energy of impact = Potential energy of the falling load σ 2 AL Energy of impact = 2E Potential energy of the falling load = P ( h + δL ) € P ⎛ €2AEh ⎞ σ = ⎜1+ 1+ ⎟ A ⎝ PL ⎠ €
  • 16. Impact Load   PROBLEM- A vertical compound tie member fixed rigidly at its upper end 20 mm consists of a steel rod 2.5 m long and 2.5 m P=10kN 30mm external diameter. The rod and 1 2 the tube are fixed together at the ends. 3 mm The compound member is then suddenly loaded in tension by a weight 21 mm of 10 kN falling through a height of 3 mm on to a flange fixed to its lower 30 mm end. Calculate the maximum stresses in steel and brass. Assume Es=2x105 N/mm2 and Eb=1.0x105 N/mm2
  • 17. Impact Load   Strain energy in shear loading. τ 2 AL Strain energy stored = 2C P D D1 C C1 € h φ φ A l B € €
  • 18. Impact Load   PROBLEM- The shear stress in a material at a price is given as 50N/mm2. Determine the local strain energy per unit volume stored in the material due to shear stress. Take C=8x104 N/mm2