Strain gauge and rosettes

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

Lecture 8 Plane Strain and Measurement of Strain

Chapter 7 Transformations of Stress and Strain

Second Order Partial Differential Equations

CHAPTER 25 SOLVING EQUATIONS BY ITERATIVE METHODS

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

2 Composition. Invertible Mappings

the total number of electrons passing through the lamp.

Example Sheet 3 Solutions

Space-Time Symmetries

derivation of the Laplacian from rectangular to spherical coordinates

Section 8.3 Trigonometric Equations

Lecture 6 Mohr s Circle for Plane Stress

Homework 3 Solutions

EE512: Error Control Coding

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

Capacitors - Capacitance, Charge and Potential Difference

Inverse trigonometric functions & General Solution of Trigonometric Equations

CHAPTER 48 APPLICATIONS OF MATRICES AND DETERMINANTS

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

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

Matrices and Determinants

Homework 8 Model Solution Section

Second Order RLC Filters

CRASH COURSE IN PRECALCULUS

The Simply Typed Lambda Calculus

4.6 Autoregressive Moving Average Model ARMA(1,1)

6.1. Dirac Equation. Hamiltonian. Dirac Eq.

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

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

A Note on Intuitionistic Fuzzy. Equivalence Relation

ST5224: Advanced Statistical Theory II

Solutions to Exercise Sheet 5

[1] P Q. Fig. 3.1

Mean bond enthalpy Standard enthalpy of formation Bond N H N N N N H O O O

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

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

Instruction Execution Times

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.

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

ADVANCED STRUCTURAL MECHANICS

Reminders: linear functions

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

2. THEORY OF EQUATIONS. PREVIOUS EAMCET Bits.

Areas and Lengths in Polar Coordinates

Mechanical Behaviour of Materials Chapter 5 Plasticity Theory

Section 8.2 Graphs of Polar Equations

Areas and Lengths in Polar Coordinates

Math 6 SL Probability Distributions Practice Test Mark Scheme

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

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

CHAPTER 101 FOURIER SERIES FOR PERIODIC FUNCTIONS OF PERIOD

6.3 Forecasting ARMA processes

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

5.4 The Poisson Distribution.

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

Mechanics of Materials Lab

Congruence Classes of Invertible Matrices of Order 3 over F 2

Math221: HW# 1 solutions

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

Section 9.2 Polar Equations and Graphs

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

ΑΚΑ ΗΜΙΑ ΕΜΠΟΡΙΚΟΥ ΝΑΥΤΙΚΟΥ ΜΑΚΕ ΟΝΙΑΣ ΣΧΟΛΗ ΜΗΧΑΝΙΚΩΝ ΠΤΥΧΙΑΚΗ ΕΡΓΑΣΙΑ

Derivation of Optical-Bloch Equations

MECHANICAL PROPERTIES OF MATERIALS

(1) Describe the process by which mercury atoms become excited in a fluorescent tube (3)

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

Potential Dividers. 46 minutes. 46 marks. Page 1 of 11

Finite Field Problems: Solutions

SCITECH Volume 13, Issue 2 RESEARCH ORGANISATION Published online: March 29, 2018

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


ΠΑΝΔΠΙΣΗΜΙΟ ΜΑΚΔΓΟΝΙΑ ΠΡΟΓΡΑΜΜΑ ΜΔΣΑΠΣΤΥΙΑΚΧΝ ΠΟΤΓΧΝ ΣΜΗΜΑΣΟ ΔΦΑΡΜΟΜΔΝΗ ΠΛΗΡΟΦΟΡΙΚΗ

Commutative Monoids in Intuitionistic Fuzzy Sets

(Mechanical Properties)

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

Ordinal Arithmetic: Addition, Multiplication, Exponentiation and Limit

Trigonometry 1.TRIGONOMETRIC RATIOS

( ) 2 and compare to M.

Other Test Constructions: Likelihood Ratio & Bayes Tests

Partial Differential Equations in Biology The boundary element method. March 26, 2013

C.S. 430 Assignment 6, Sample Solutions

Jesse Maassen and Mark Lundstrom Purdue University November 25, 2013

1 String with massive end-points

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

2. Μηχανικό Μαύρο Κουτί: κύλινδρος με μια μπάλα μέσα σε αυτόν.

Calculating the propagation delay of coaxial cable

Spherical Coordinates

Statistical Inference I Locally most powerful tests

SCHOOL OF MATHEMATICAL SCIENCES G11LMA Linear Mathematics Examination Solutions

D Alembert s Solution to the Wave Equation

Διπλωματική Εργασία του φοιτητή του Τμήματος Ηλεκτρολόγων Μηχανικών και Τεχνολογίας Υπολογιστών της Πολυτεχνικής Σχολής του Πανεπιστημίου Πατρών

SOLUTIONS TO MATH38181 EXTREME VALUES AND FINANCIAL RISK EXAM

( y) Partial Differential Equations

Written Examination. Antennas and Propagation (AA ) April 26, 2017.

Solution Series 9. i=1 x i and i=1 x i.

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

MathCity.org Merging man and maths

Fractional Colorings and Zykov Products of graphs

Transcript:

Strain gauge and rosettes Introduction A strain gauge is a device which is used to measure strain (deformation) on an object subjected to forces. Strain can be measured using various types of devices classified depending upon their principle of operation. Some of them are as follows: 1. Mechanical type,. Optical type 3. Pneumatic type 4. Electrical type Earlier, mechanical type of device such as extensometer or extension meter was used to measure strain by measuring change in length. Photoelectric strain gauge was also introduced which uses a light beam to produce electric current corresponding to deformation. The most commonly used strain gauge is an electrical resistance strain gauge. This strain gauge works on the principle that when a metallic wire type gauge is strained (here due to forces on object in contact), the resistance of the wire will be changed due to changes in its length, diameter and resistivity. Resistance (R) = ρl A Where ρ is resistivity; L is length of wire; A is area of crossection of wire. This change in resistance will be in proportion with the strain produced which can be easily measured using Wheatstone bridge.

Drawbacks of Strain gauge 1. A strain gauge is capable only of measuring strain in the direction in which gauge is oriented.. There is no direct way to measure the shear strain or to directly measure the principal strains as directions of principal planes are not generally known. Strain rosettes Since for strain analysis in biaxial state of stress we should know strain in three directions and due to drawbacks in a strain gauge, Strain rosettes came in to picture. Strain rosette can be defined as the arrangement of strain gauges in three arbitrary directions. These strain gauges are used to measure the normal strain in those three directions. Depending on the arrangement of strain gauges, strain rosettes are classified in to:- 1. Rectangular strain gauge rosette. Delta strain gauge rosette 3. Star strain gauge rosette Rectangular strain gauge rosette A rectangular strain rosette consists of three strain gauges arranged as follows:- Y C c X 45 45 A

We know normal strain in any direction (θ) is given by ε n = 1 (ε x + εy) + 1 (εx εy) cos θ + γ xy Sin θ where ε x = normal strain at a point in x-direction εy = normal strain at a point in y- direction γ xy = shear strain at a point on x face in y direction So, normal strain at θ = 0 ε A = (ε n ) θ=0 = 1 (ε x + εy) + 1 (εx εy) cos 0 + γ xy ε A = (ε n ) θ=0 = 1 (ε x + εy) + 1 (εx εy) ε A = (ε n ) θ=0 = ε x Eqn (1) Sin 0 Normal strain at θ = 45 (with respect to strain guage A, anticlockwise) ε B = (ε n ) θ=45 = 1 (ε x + εy) + 1 (εx εy) cos 90 + γ xy ε B = (ε n ) θ=45 = 1 (ε x + εy) + γ xy ε x + εy + γ xy = ε B Eqn () Sin 90 Similarly, normal strain at θ= 90 (with respect to strain guage A, anticlockwise) ε c = (ε n ) θ=90 = 1 (ε x + εy) + 1 (εx εy) cos 180 + γ xy Sin 180

ε c = (ε n ) θ=90 = 1 (ε x + εy) - 1 (εx εy) εc = (ε n ) θ=90 = ε y Eqn (3) From Eqn 1, and 3 γ xy = ε B ε A εc Note :- With the help of rectangular strain rosette we get strains in three arbitrary directions which in turn give us ε x, εy and γ xy and hence principal strains at a point on the surface of the object can be determined. Delta strain gauge rosette A delta strain gauge also consist of three strain gauges arranged as shown below 60 A 10 Delta strain gauge rosette ε A = (ε n ) θ=0 ε B = (ε n ) θ=60 εc = (ε n ) θ=10

We know normal strain in any direction (θ) is given by ε n = 1 (ε x + εy) + 1 (εx εy) cos θ + γ xy So, normal strain at θ = 0 Sin θ ε A = (ε n ) θ=0 = 1 (ε x + εy) + 1 (εx εy) cos 0 + γ xy ε A = (ε n ) θ=0 = 1 (ε x + εy) + 1 (εx εy) ε A = (ε n ) θ=0 = ε x Eqn (4) Sin 0 Normal strain at θ = 60 (with respect to strain gauge A, anticlockwise) ε B = (ε n ) θ=60 = 1 (ε x + εy) + 1 (εx εy) cos 10 + γ xy Eqn (5) Sin 10 Similarly, normal strain at θ= 10 (with respect to strain gauge A, anticlockwise) εc = (ε n ) θ=10 = 1 (ε x + εy) + 1 (εx εy) cos 40 + γ xy Eqn (6) Sin 40 Similarly, ε x, εy and γ xy can be determined from equations 4, 5 and 6 and hence principal strains at a point on the surface of the object. Star strain gauge rosette This rosette consist of three strain gauges in three directions as shown below

10 40 A Star strain gauge rosette ε A = (ε n ) θ=0 ε B = (ε n ) θ=10 εc = (ε n ) θ=40 We know normal strain in any direction (θ) is given by ε n = 1 (ε x + εy) + 1 (εx εy) cos θ + γ xy So, normal strain at θ = 0 Sin θ ε A = (ε n ) θ=0 = 1 (ε x + εy) + 1 (εx εy) cos 0 + γ xy ε A = (ε n ) θ=0 = 1 (ε x + εy) + 1 (εx εy) ε A = (ε n ) θ=0 = ε x Eqn (7) Sin 0 Normal strain at θ = 10 (with respect to strain gauge A, anticlockwise)

ε B = (ε n ) θ=10 = 1 (ε x + εy) + 1 (εx εy) cos 40 + γ xy Eqn (8) Sin 40 Similarly, normal strain at θ= 40 (with respect to strain gauge A, anticlockwise) εc = (ε n ) θ=40 = 1 (ε x + εy) + 1 (εx εy) cos 480 + γ xy Eqn (9) Sin 480 Similarly, by solving equations 7, 8 and 9 we can determine ε x, εy and γ xy and hence principal strains at a point on the surface of the object. Sample Question for Concept brush-up S-1. Determine maximum shear stress at a point by using the following strain gauge readings of rectangular strain rosette ε 0 = 400 * 10-6 Young s Modulus = E= 00 GPa ε 45 = 375 * 10-6 Poisson ratio = 0.5 ε 90 = 00 * 10-6 Solution : We know from Eqn 1, and 3 ε A = (ε n ) θ=0 = ε x = 400 * 10-6 ε c = (ε n ) θ=90 = ε y = 00 * 10-6 ε B = (ε n ) θ=45 = 375 * 10-6 and ε x + εy + γ xy = ε B

γ xy = 150 * 10-6 Principal strain, ε 1, = 1 [( ε x + ε y ) ± ( ) ( ) ] ε 1 = 45 * 10-6 ε = 175 * 10-6 Principal stress, 1 = E 1-µ ( ε 1 + µ ε ) 1 = 100 Mpa = E 1-µ ( ε + µ ε 1 ) = 60 Mpa Absolute τ max = 1 Or 1 - As principal stresses like in nature therefore Ans. Absolute τ max = 1 = 50 Mpa References 1. Mechanics of Materials by B.C. Punmia. Strength of Materials by R.K. Bansal