# MECHANICS OF MATERIALS

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1 Third E CHAPTER 2 Stress MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University and Strain Axial Loading

2 Contents Stress & Strain: Axial Loading Normal Strain Stress-Strain Test Stress-Strain Diagram: Ductile Materials Stress-Strain Diagram: Brittle Materials Hooke s Law: Modulus of Elasticity Elastic vs. Plastic Behavior Fatigue Deformations Under Axial Loading Example 2.01 Sample Problem 2.1 Static Indeterminacy Example 2.04 Thermal Stresses Poisson s Ratio Generalized Hooke s Law Dilatation: Bulk Modulus Shearing Strain Example 2.10 Relation Among E, ν, and G Sample Problem 2.5 Composite Materials Saint-Venant s Principle Stress Concentration: Hole Stress Concentration: Fillet Example 2.12 Elastoplastic Materials Plastic Deformations Residual Stresses Example 2.14, 2.15,

3 Stress & Strain: Axial Loading Suitability of a structure or machine may depend on the deformations in the structure as well as the stresses induced under loading. Statics analyses alone are not sufficient. Considering structures as deformable allows determination of member forces and reactions which are statically indeterminate. Determination of the stress distribution within a member also requires consideration of deformations in the member. Chapter 2 is concerned with deformation of a structural member under axial loading. Later chapters will deal with torsional and pure bending loads. 2-3

4 Normal Strain 2-4

5 Stress-Strain Test 2-5

6 Stress-Strain Diagram: Ductile Materials 2-6

7 Stress-Strain Diagram: Brittle Materials 2-7

8 Hooke s Law: Modulus of Elasticity Below the yield stress Strength is affected..,., and.. but. (Modulus of Elasticity) is not. 2-8

9 Elastic vs. Plastic Behavior elastically. elastic limit.. plastically. 2-9

10 Fatigue....fatigue at stress levels significantly below the.if subjected to many. When the stress is reduced below the., fatigue failures do not occur for any number of cycles. 2-10

11 Deformations Under Axial Loading From Hooke s Law: From the definition of strain: Equating and solving for the deformation, With variations in loading, cross-section or material properties, 2-11

12 Example 2.01 E D 1.07 in. psi d in. Determine the deformation of the steel rod shown under the given loads. SOLUTION:

13 SOLUTION: Divide the rod into three components: Apply free-body analysis to each component to determine internal forces, Evaluate total deflection, L 1 A 1 L A in. 0.9 in 2 L A in. 0.3 in

14 Sample Problem 2.1 SOLUTION: The rigid bar BDE is supported by two links AB and CD. Link AB is made of aluminum (E 70 GPa) and has a cross-sectional area of 500 mm 2. Link CD is made of steel (E 200 GPa) and has a cross-sectional area of (600 mm 2 ). For the 30-kN force shown, determine the deflection a) of B, b) of D, and c) of E

15 Sample Problem 2.1 SOLUTION: Free body: Bar BDE Displacement of B: Displacement of D: 2-15

16 Sample Problem 2.1 Displacement of D: 2-16

17 Static Indeterminacy.. statically indeterminate

18 Example 2.04 SOLUTION:

19 Example 2.04 SOLUTION: Solve for the displacement at B due to the applied loads with the redundant constraint released, Solve for the displacement at B due to the redundant constraint, 2-19

20 Example 2.04 Require that the displacements due to the loads and due to the redundant reaction be compatible, Find the reaction at A due to the loads and the reaction at B 2-20

21 Thermal Stresses thermal strain

22 Poisson s Ratio For a slender bar subjected to axial loading:.. Poisson s ratio is defined as 2-22

23 Generalized Hooke s Law. principle of superposition. This requires: 1). 2). With these restrictions: 2-23

24 Dilatation: Bulk Modulus Relative to the unstressed state, the change in volume is e dilatation (...) For element subjected to uniform hydrostatic pressure, Subjected to uniform pressure, dilatation must be negative, therefore

25 Shearing Strain.., τ xy ( ) f γ xy τ G... τ G... τ G... xy yz zx where G is the.or

26 Example 2.10 A rectangular block of material with modulus of rigidity G 90 ksi is bonded to two rigid horizontal plates. The lower plate is fixed, while the upper plate is subjected to a horizontal force P. Knowing that the upper plate moves through 0.04 in. under the action of the force, determine a) the average shearing strain in the material, and b) the force P exerted on the plate. SOLUTION:

27 Determine the average angular deformation or shearing strain of the block. Apply Hooke s law for shearing stress and strain to find the corresponding shearing stress. Use the definition of shearing stress to find the force P. 2-27

28 Relation Among E, ν, and G An axially loaded slender bar will elongate in the axial direction and contract in the transverse directions. An initially cubic element oriented as in top figure will deform into a rectangular parallelepiped. The axial load produces a normal strain. If the cubic element is oriented as in the bottom figure, it will deform into a rhombus. Axial load also results in a shear strain. Components of normal and shear strain are related, 2-28

29 Sample Problem 2.5 A circle of diameter d 9 in. is scribed on an unstressed aluminum plate of thickness t 3/4 in. Forces acting in the plane of the plate later cause normal stresses σ x 12 ksi and σ z 20 ksi. For E 10x10 6 psi and ν 1/3, determine the change in: a) the length of diameter AB, b) the length of diameter CD, c) the thickness of the plate, and d) the volume of the plate. 2-29

30 SOLUTION: Apply the generalized Hooke s Law to find the three components of normal strain. Evaluate the deformation components. ε ε ε x y z δ B A δ C D...in....in....in. Find the change in volume δ t 3 V...in 2-30

31 Composite Materials Fiber-reinforced composite materials are formed from lamina of fibers of graphite, glass, or polymers embedded in a resin matrix. Normal stresses and strains are related by Hooke s Law but with directionally dependent moduli of elasticity, E x ν σ x ε xy x ε y ε x E y ν σ ε xz y y ε z ε x E z σ z ε Transverse contractions are related by directionally dependent values of Poisson s ratio, e.g., Materials with directionally dependent mechanical properties are anisotropic. z 2-31

32 Saint-Venant s Principle Loads transmitted through rigid plates result in uniform distribution of stress and strain. Concentrated loads result in large stresses in the vicinity of the load application point. Stress and strain distributions become uniform at a relatively short distance from the load application points. Saint-Venant s Principle: Stress distribution may be assumed independent of the mode of load application except in the immediate vicinity of load application points. 2-32

33 Stress Concentration: Hole Discontinuities of cross section may result in high localized or concentrated stresses. K σ σ max ave 2-33

34 Stress Concentration: Fillet 2-34

35 Example 2.12 SOLUTION: Determine the largest axial load P that can be safely supported by a flat steel bar consisting of two portions, both 10 mm thick, and respectively 40 and 60 mm wide, connected by fillets of radius r 8 mm. Assume an allowable normal stress of 165 MPa. Determine the geometric ratios and find the stress concentration factor from Fig. 2.64b. Find the allowable average normal stress using the material allowable normal stress and the stress concentration factor. Apply the definition of normal stress to find the allowable load. 2-35

36 Determine the geometric ratios and find the stress concentration factor from Fig. 2.64b. D d 60mm mm K 1.82 r d 8mm 40mm 0.20 Find the allowable average normal stress using the material allowable normal stress and the stress concentration factor. σ σ K 165MPa 1.82 max ave 90.7 MPa Apply the definition of normal stress to find the allowable load. P Aσ ( 40mm)( 10mm)( 90.7 MPa) ave N P 36.3kN 2-36

37 Elastoplastic Materials Previous analyses based on assumption of linear stress-strain relationship, i.e., stresses below the yield stress Assumption is good for brittle material which rupture without yielding If the yield stress of ductile materials is exceeded, then plastic deformations occur Analysis of plastic deformations is simplified by assuming an idealized elastoplastic material Deformations of an elastoplastic material are divided into elastic and plastic ranges Permanent deformations result from loading beyond the yield stress 2-37

38 Plastic Deformations A P σ ave A σ max K σ P Y A Y K Elastic deformation while maximum stress is less than yield stress Maximum stress is equal to the yield stress at the maximum elastic loading P U σ A Y K P Y At loadings above the maximum elastic load, a region of plastic deformations develop near the hole As the loading increases, the plastic region expands until the section is at a uniform stress equal to the yield stress 2-38

39 Residual Stresses When a single structural element is loaded uniformly beyond its yield stress and then unloaded, it is permanently deformed but all stresses disappear. This is not the general result. Residual stresses will remain in a structure after loading and unloading if - only part of the structure undergoes plastic deformation - different parts of the structure undergo different plastic deformations Residual stresses also result from the uneven heating or cooling of structures or structural elements 2-39

40 Example 2.14, 2.15, 2.16 A cylindrical rod is placed inside a tube of the same length. The ends of the rod and tube are attached to a rigid support on one side and a rigid plate on the other. The load on the rod-tube assembly is increased from zero to 5.7 kips and decreased back to zero. a) draw a load-deflection diagram for the rod-tube assembly b) determine the maximum elongation c) determine the permanent set d) calculate the residual stresses in the rod and tube. A E σ r r Y, r 0.075in ksi 2 psi A E σ t t Y, t 0.100in ksi 2 psi 2-40

41 Example 2.14, 2.15, 2.16 a) draw a load-deflection diagram for the rodtube assembly P Y, r σ Y, r A r 2 ( 36ksi)( 0.075in ) 2.7 kips δ Y,r ε Y, r L σ E Y, r Y, r L psi 30in psi -3 in. P Y, t σ Y, t A t 2 ( 45ksi)( 0.100in ) 4.5kips δ Y,t ε Y, t L σ E Y, t Y, t L psi 30in psi -3 in. P P r + P t δ δ δ r t 2-41

42 Example 2.14, 2.15, 2.16 b,c) determine the maximum elongation and permanent set at a load of P 5.7 kips, the rod has reached the plastic range while the tube is still in the elastic range P P r t σ t P Y, r P P Pt A t 2.7 kips r ( ) 3.0 kips 30ksi 2 0.1in kips 3.0 kips δ t ε L t σ t E t L psi 30in. psi δ max δ t in. the rod-tube assembly unloads along a line parallel to 0Y r 4.5kips m 125kips in. slope in. P δ m max 5.7 kips kips in. 3 in. δ p δ max + δ 3 ( ) 10 in. δ p in. 2-42

43 Example 2.14, 2.15, 2.16 calculate the residual stresses in the rod and tube. calculate the reverse stresses in the rod and tube caused by unloading and add them to the maximum stresses. δ ε L in. 3 in in. in. σ r σ t ε E ε E t r 3 6 ( )( psi) 3 6 ( )( psi) 45.6 ksi 22.8ksi σ σ residual, r residual, t σ + σ σ + σ t r t r ( ) ksi 9. 6ksi ( ) ksi 7.2ksi 2-43

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