Matrices Review. Here is an example of matrices multiplication for a 3x3 matrix

Σχετικά έγγραφα
σ zz Stresses in 3-D σ yy τ yx σ xx z τ zy τ zx τ yz τ xz τ xy

Lecture 6 Mohr s Circle for Plane Stress

Matrices and Determinants

CHAPTER 25 SOLVING EQUATIONS BY ITERATIVE METHODS

Lecture 5 Plane Stress Transformation Equations

CHAPTER 48 APPLICATIONS OF MATRICES AND DETERMINANTS

EE512: Error Control Coding

Strain gauge and rosettes

Chapter 7 Transformations of Stress and Strain

Stresses in a Plane. Mohr s Circle. Cross Section thru Body. MET 210W Mohr s Circle 1. Some parts experience normal stresses in

Homework 8 Model Solution Section

Second Order Partial Differential Equations

Section 8.3 Trigonometric Equations

3.4 SUM AND DIFFERENCE FORMULAS. NOTE: cos(α+β) cos α + cos β cos(α-β) cos α -cos β

Απόκριση σε Μοναδιαία Ωστική Δύναμη (Unit Impulse) Απόκριση σε Δυνάμεις Αυθαίρετα Μεταβαλλόμενες με το Χρόνο. Απόστολος Σ.

Reminders: linear functions

Homework 3 Solutions

HOMEWORK 4 = G. In order to plot the stress versus the stretch we define a normalized stretch:

SCHOOL OF MATHEMATICAL SCIENCES G11LMA Linear Mathematics Examination Solutions

Dr. D. Dinev, Department of Structural Mechanics, UACEG

Exercises 10. Find a fundamental matrix of the given system of equations. Also find the fundamental matrix Φ(t) satisfying Φ(0) = I. 1.

Areas and Lengths in Polar Coordinates

Phys460.nb Solution for the t-dependent Schrodinger s equation How did we find the solution? (not required)

Areas and Lengths in Polar Coordinates

2. THEORY OF EQUATIONS. PREVIOUS EAMCET Bits.

2 Composition. Invertible Mappings

Mock Exam 7. 1 Hong Kong Educational Publishing Company. Section A 1. Reference: HKDSE Math M Q2 (a) (1 + kx) n 1M + 1A = (1) =

MATHEMATICS. 1. If A and B are square matrices of order 3 such that A = -1, B =3, then 3AB = 1) -9 2) -27 3) -81 4) 81

Macromechanics of a Laminate. Textbook: Mechanics of Composite Materials Author: Autar Kaw

Example Sheet 3 Solutions

( y) Partial Differential Equations

Trigonometry 1.TRIGONOMETRIC RATIOS

Chapter 6: Systems of Linear Differential. be continuous functions on the interval

Concrete Mathematics Exercises from 30 September 2016

ANSWERSHEET (TOPIC = DIFFERENTIAL CALCULUS) COLLECTION #2. h 0 h h 0 h h 0 ( ) g k = g 0 + g 1 + g g 2009 =?

Solutions to Exercise Sheet 5

Inverse trigonometric functions & General Solution of Trigonometric Equations

Chapter 2. Stress, Principal Stresses, Strain Energy

Introduction to Theory of. Elasticity. Kengo Nakajima Summer

( ) 2 and compare to M.

Jesse Maassen and Mark Lundstrom Purdue University November 25, 2013

Lecture 2: Dirac notation and a review of linear algebra Read Sakurai chapter 1, Baym chatper 3

derivation of the Laplacian from rectangular to spherical coordinates

1 String with massive end-points

Section 7.6 Double and Half Angle Formulas

Numerical Analysis FMN011

= l. = l. (Hooke s Law) Tensile: Poisson s ratio. σ = Εε. τ = G γ. Relationships between Stress and Strain

Approximation of distance between locations on earth given by latitude and longitude

DESIGN OF MACHINERY SOLUTION MANUAL h in h 4 0.

k A = [k, k]( )[a 1, a 2 ] = [ka 1,ka 2 ] 4For the division of two intervals of confidence in R +

Tridiagonal matrices. Gérard MEURANT. October, 2008

ST5224: Advanced Statistical Theory II

Finite Field Problems: Solutions

Quadratic Expressions

CYLINDRICAL & SPHERICAL COORDINATES

6.3 Forecasting ARMA processes

Mechanics of Materials Lab

6.1. Dirac Equation. Hamiltonian. Dirac Eq.

w o = R 1 p. (1) R = p =. = 1

Econ 2110: Fall 2008 Suggested Solutions to Problem Set 8 questions or comments to Dan Fetter 1

CHAPTER 101 FOURIER SERIES FOR PERIODIC FUNCTIONS OF PERIOD

4.6 Autoregressive Moving Average Model ARMA(1,1)

9.09. # 1. Area inside the oval limaçon r = cos θ. To graph, start with θ = 0 so r = 6. Compute dr

ΚΥΠΡΙΑΚΗ ΕΤΑΙΡΕΙΑ ΠΛΗΡΟΦΟΡΙΚΗΣ CYPRUS COMPUTER SOCIETY ΠΑΓΚΥΠΡΙΟΣ ΜΑΘΗΤΙΚΟΣ ΔΙΑΓΩΝΙΣΜΟΣ ΠΛΗΡΟΦΟΡΙΚΗΣ 6/5/2006

TMA4115 Matematikk 3

ΚΥΠΡΙΑΚΗ ΕΤΑΙΡΕΙΑ ΠΛΗΡΟΦΟΡΙΚΗΣ CYPRUS COMPUTER SOCIETY ΠΑΓΚΥΠΡΙΟΣ ΜΑΘΗΤΙΚΟΣ ΔΙΑΓΩΝΙΣΜΟΣ ΠΛΗΡΟΦΟΡΙΚΗΣ 19/5/2007

Chapter 6: Systems of Linear Differential. be continuous functions on the interval

Practice Exam 2. Conceptual Questions. 1. State a Basic identity and then verify it. (a) Identity: Solution: One identity is csc(θ) = 1

Pg The perimeter is P = 3x The area of a triangle is. where b is the base, h is the height. In our case b = x, then the area is

Second Order RLC Filters

b. Use the parametrization from (a) to compute the area of S a as S a ds. Be sure to substitute for ds!

Math221: HW# 1 solutions

Srednicki Chapter 55

CRASH COURSE IN PRECALCULUS

PARTIAL NOTES for 6.1 Trigonometric Identities

Trigonometric Formula Sheet

Problem Set 9 Solutions. θ + 1. θ 2 + cotθ ( ) sinθ e iφ is an eigenfunction of the ˆ L 2 operator. / θ 2. φ 2. sin 2 θ φ 2. ( ) = e iφ. = e iφ cosθ.

ΚΥΠΡΙΑΚΗ ΕΤΑΙΡΕΙΑ ΠΛΗΡΟΦΟΡΙΚΗΣ CYPRUS COMPUTER SOCIETY ΠΑΓΚΥΠΡΙΟΣ ΜΑΘΗΤΙΚΟΣ ΔΙΑΓΩΝΙΣΜΟΣ ΠΛΗΡΟΦΟΡΙΚΗΣ 24/3/2007

= λ 1 1 e. = λ 1 =12. has the properties e 1. e 3,V(Y

The Simply Typed Lambda Calculus

Appendix to On the stability of a compressible axisymmetric rotating flow in a pipe. By Z. Rusak & J. H. Lee

D Alembert s Solution to the Wave Equation

forms This gives Remark 1. How to remember the above formulas: Substituting these into the equation we obtain with

Lecture 8 Plane Strain and Measurement of Strain

Math 6 SL Probability Distributions Practice Test Mark Scheme

Notes on the Open Economy

MATRICES

Integrals in cylindrical, spherical coordinates (Sect. 15.7)

ADVANCED STRUCTURAL MECHANICS

ECE Spring Prof. David R. Jackson ECE Dept. Notes 2

SOLUTIONS TO MATH38181 EXTREME VALUES AND FINANCIAL RISK EXAM

Exercises to Statistics of Material Fatigue No. 5

Spherical Coordinates

Other Test Constructions: Likelihood Ratio & Bayes Tests

5.4 The Poisson Distribution.

Congruence Classes of Invertible Matrices of Order 3 over F 2

C.S. 430 Assignment 6, Sample Solutions

Differentiation exercise show differential equation

Durbin-Levinson recursive method

If we restrict the domain of y = sin x to [ π, π ], the restrict function. y = sin x, π 2 x π 2

Transcript:

Matrices Review Matri Multiplication : When the number of columns of the first matri is the same as the number of rows in the second matri then matri multiplication can be performed. Here is an eample of matri multiplication for two matrices Here is an eample of matrices multiplication for a matri When A has dimensions mn, B has dimensions np. Then the product of A and B is the matri C, which has dimensions mp.

Transpose of Matrices : The transpose of a matri is found b echanging rows for columns i.e. Matri A (aij) and the transpose of A is: A T (aij) Where i is the row number and j is the column number. For eample, The transpose of a matri would be: n the case of a square matri (mn), the transpose can be used to chec if a matri is smmetric. For a smmetric matri A A T

The Determinant of a Matri : Determinants pla an important role in finding the inverse of a matri and also in solving sstems of linear equations. Determinant of a matri Assuming A is an arbitrar matri A, where the elements are given b: Determinant of a matri The determinant of a matri is more difficult

nverse Matri For a matri the matri inverse is Eample: Cos A Sin Sin Cos A A Cos Sin Cos Sin Sin Cos Sin Cos A T A Cos Sin For a matri

XY Y X X ( ) [T ] Coordinate Transformations T ] [ ] [ T XY Y X Y

Theor of Matri Method for Stress Calculations in -D From equations of rotational transformation of ais, we obtain the following: T inversel Hence T Y T Y T AC Area A AB A BC A A X X B C

Ug and force equilibrium equation, we obtain epressions for stress transformations as follows: {} Σ{ F} F F F {} F F F AB BC AC {} A A A A {} A A Canceling area A out and pre-multipling b transformation T (where T T T the identit matri. The order of the matri multiplication does matter in the final outcome., we have

{} A A

For the forces in the X ais we will use the same procedure. Y Y X X B C D BD Area A BC A CD A { } { } {} {} {} Σ BD BC CD A A A A A A F F F F F F F

Combining the above epressions T T T or

State of Stresses in Three Dimensions K The general three dimensional state of stress consists of three unequal principal stresses acting at a point (triaial state of stresses). L The plane JKL is assumed to be a principal plane and is the principal stress acting normal to the plane. - J - Letα, β and γ are the angles between the vector and the, and ais respectivel and α l β m γ

Under equilibrium conditions ( ) ( ) l l l m m ( ) m l m l m l l l m m m As, l and m are different than ero (non-trivial solution) l m The determinant must be equal to ero Solution of the determinant results in a cubic equation in

The eigenvalues of the stress matri are the principal stresses. The eigenvectors of the stress matri are the principal directions. m l > > m l The three roots are the three principal stresses,,.,, and are nown as stress invariants as the do not change in value when the aes are rotated to new positions.

has been seen before for the two dimensional state of stress. t states the useful relationship that the sum of the normal stresses for an orientation in the coordinate sstem is equal to the sum of the normal stresses for an other orientation

( ) 6, A A ± α α ( ) ( ) A Cos A α Stress nvariants for Principal Stresses,, ma ma The solution are the eigenvalues of the stress tensor

Eample: determine the principal stresses for the state of stress (in MPa). Solution: The solution are the eigenvalues of the stress tensor; Substituting: ( 4) ( 4) ( 8) 4 4 ( ( 8) ) ( ( ( ) ) (( 4) ( 4)) ) 8 One solution -8MPa is a principal stress because and are ero, then the other two principal stresses are eas to find b solving the quadratic equation inside the square bracets for (4) ± 6 ( ) ± ( ) 4(4) 6MPa -6MPa

4 4 8 8,6 6,8, A 96.4 96.4Cos 96.4Cos 96.4Cos Cos(α ) (.5).86 8 (.5 6) 59.99 8 8 α.5 6. (.5 6) 79. 9 6 6 8

Eample : Determine the maimum principal stresses and the maimum shear stress for the following triaial stress state. Solution Stress _ Tensor [ ] 4 4 4 MPa 4 5 4 5 5-5 MPa 5 MPa -895 MPa

Solution to Eample 6-5.8 MPa 4 6.5 MPa Sigm a (MPa) - -8-6 -4-4 6 8-65. MPa -4-6 -8 Stress (MPa) ma 65.MPa / (65. 6.5MPa 5.8) 58.5MPa 5.8MPa

Mohr s Circles for -D Analsis Mohr s circles can mae visualiation of the stress condition clearer to the designer. Note that the principal stress values are alwas ordered b convention so the is the largest value in the tensile direction and is the largest value in the compressive direction. Note also that there is one dominant pea shear stress in this diagram. Be forewarned the principal stresses and this pea shear stress are going to pla a strong role in determining the factor of safet in mechanical design.

A Mohr s circle can be generated for triaial stress states, but it is often unnecessar, as it is sufficient to now the values of the principal stresses. The principal stresses must be ordered from larger to smaller.

Compare -D and -D Mohr s Circle. f is ero, does it have an effect in D?

Q P α α Consider then the plane will be an angle α from, in the direction of (clocwise). Point P Consider then the plane will be an angle α from, in the direction of (clocwise). Point Q The required sstem of stresses, fall within P and Q. Loci determined b the center in

β β Consider then the plane will be an angle β from, in the direction of (anticlocwise). Point R Consider then the plane will be an angle β from, in the direction of (clocwise). Point S The required sstem of stresses, fall within R and S. Loci determined b the center in

Eample: Use Mohr s Circle to obtain the principal stresses and maimum shear of a component subjected to the following stresses: 9tension tension 5compression 4ccw ccw counterclocwise

Stress on ANY nclined Plane (-D) S The stress on a plane (S) can be decomposed into its normal component (S n ) and its shear component (S s ). S S n s S s s n s f α, β and γ are the angles between the vector S n and the, and ais respectivel and α l β m γ then

[ ] [ ] T T T t can be proved that

Mohr s Circles for -D Analsis There is no eas Mohr s circle graphical solution for problems of triaial stress state. Solution for maimum principal stresses and maimum shear stress is analtical. Consider the, and ais to coincide with the ais of the principal stresses, and. f α, β and γ are the angles between the normal to the plane and the, and ais respectivel and α l β m l m γ We would lie to find graphicall the normal stress and shear stress on the plane.

Octahedral Plane and Stresses An octahedral plane is a plane that maes three identical angles with the principal planes. ( ) ( ) ( ) ( ) 6 9 n n n n n n n n op op op op m l m m l l m l

Mean and Deviatoric Stresses When describing the materials behavior of metals, one concludes that in certain cases some stress components pla a more important role than other components. Plastic behavior of metals, is reported to be independent of the average (mean) normal stress. M M M op M M Mean stress matri Deviatoric stress M M M The shear components do not change

D Deviatoric Stress Matri Deviatoric stresses pla an important role in the theor of plasticit. The influence the ielding of ductile materials. The principal stresses obtained onl from the deviatoric matri is M M M D P,

Eample For a given stress matri representing the state of stress at a certain point [ ] MPa Find the stress invariant, the principal stresses, the principal directions, the octahedral stress and the shear stress associated with the octahedral stress. Solution: 5 5 5 5.4. 5.4

( ) ( ) ( ) 5.4 5.4 5.4 m l m l m l.4. 5.4 [ ] MPa ( ) ( ) ( ) m l m l m l.67.48.657 m l m l.555.8 m l.546.64.74 m l 5 Mean 9 8 8 5) ( 6 5 9 6 9 op op op