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HANOI UNIVERSITY OF SCIENCE AND TECHNOLOGY UNIVERSITY OF MECHANICS Finite Element Methods Preparedby Prof.M.C. Nguyen, Dept of Mechatronics 1
HANOI UNIVERSITY OF SCIENCE AND TECHNOLOGY UNIVERSITY OF MECHANICS Finite Element Methods Preparedby Prof.M.C. Nguyen, Dept of Mechatronics 1
UNIT - 1 • Introduction to FEM: – Stiffness equations for a axial bar element in local co-ordinates using Potential Energy approach and Virtual energy principle – Finite element analysis of uniform, stepped and tapered bars subjected to mechanical and thermal loads – Assembly of Global stiffness matrix and loadvector – Quadratic shape functions – properties of stiffness matrix 2
Axially Loaded Bar –GoverningEquations and Boundary Conditions • Differential Equation d EA(x) du f (x) 0 0 x L dx dx • Boundary Condition Types • prescribed displacement (essential BC) •prescribed force/derivative of displacement (natural BC) 5
Potential Energy • Elastic Potential Energy (PE) - Spring case Unstretched spring PE 0 Stretchedbar 1 PE kx2 2 x - Axially loaded bar undeformed: PE 0 1 L deformed: PE Adx 2 - Elastic body 0 PE 1 σT εdv 2 V 7
Potential Energy • Work Potential (WE) f P f: distributed force over a line A B P: point force L u: displacement WP u fdx PuB 0 • Total Potential Energy 1 L L Adx u fdx Pu B 2 0 0 • Principle of Minimum PotentialEnergy For conservative systems, of all the kinematically admissible displacement fields, those corresponding to equilibrium extremize the total potential energy. If the extremum condition is a minimum, the equilibrium state isstable. 8
Potential Energy + Rayleigh-Ritz Approach Example: f P A B Step 1: assume a displacement field u a x i 1 to n i i i is shape function / basis function n is the order of approximation Step 2: calculate total potential energy 9
Potential Energy +Rayleigh-Ritz Approach Example: f P A B Step 3:select ai so that the total potential energy isminimum 10
Galerkin’sMethod Example: f P A B d du Seekan approximation u~so EA(x) f (x) 0 dx dx d du~ ux 0 0 wi EA(x) f ( x)dV 0 dx dx V EA(x) du P u~x 0 0 dx du~ xL EA(x) P dx xL In the Galerkin’s method, the weight function is chosen to be the same as the shape function. 11
Galerkin’sMethod Example: f P A B d du~ L du~dw L du~L wi EA(x) f ( x)dV 0 EA(x) i dx wi fdx wi EA(x) 0 dx dx dx dx dx V 0 0 0 1 2 3 1 2 3 12
FEM Formulation of AxiallyLoaded Bar –Governing Equations • Differential Equation d du EA(x) f (x) 0 0 x L dx dx • Weighted-Integral Formulation L w d EA(x) du f (x)dx 0 0 dx dx • Weak Form L L dw du du 0 EA(x) wf (x)dx wEA(x) dx dx dx 0 0 14
Approximation Methods –Finite Element Method Example: Step 1: Discretization Step 2: Weak form of one element P P 1 2 x1 x 2 x x2 dw du du 2 dx EA(x) dx w(x) f (x)dx w(x)EA(x) dx 0 x x1 1 x2 dw du EA(x) w(x) f (x)dx w x P w x P 0 dx dx 2 2 1 1 x1 15
Approximation Methods –Finite Element Method Example (cont): Step 3: Choosing shape functions - linear shapefunctions u u u 1 1 2 2 x x l x 1 2 x x x x 1 1 2 ; 1 ; 1 2 2 2 1 l 2 l 2 1l x x 1; x x l 1 2 1 16
Approximation Methods –Finite Element Method Example (cont): Step 4: Forming element equation E,Aare constant EA EA x2 x2 1 u u x2 Letw , weak form becomes EA 2 1 dx f dx P P 0 u u f dx P 1 l 1 l 2 1 1 l l 1 1 2 1 1 x1 x1 x1 EA EA x2 x2 1 u u x2 Letw , weak form becomes EA 2 1 dx f dx P P 0 u u f dx P 2 l 1 l 2 2 2 l l 2 2 2 2 1 x1 x1 x1 x2 1 fdx EA 1 1u x P f P 1 1 1 1 1 l 1 1 u x2 P f P 2 fdx 2 2 2 2 x1 17
Approximation Methods –Finite Element Method Example (cont): Step 5: Assembling to form systemequation Approach 1: 1 1 0 0 uI f I PI 1 1 1 Element 1: E AI I 1 1 0 0uI f I PI 2 2 2 lI 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Element2: E II AII 0 1 1 0 uII f II PII 1 1 1 lII 0 1 1 0uII f II PII 0 0 0 2 2 2 0 0 0 0 0 0 0 0 0 0 0 Element 3: E III AIII 0 0 0 0 0 0 0 lIII 0 0 1 1 u III f III PIII 1 1 1 18 0 0 1 1 uIII f III PIII 2 2 2
Approximation Methods –Finite Element Method Example (cont): Step 5: Assembling to form systemequation Assembled System: E A E AI I I I 0 0 lI lI II II u f P I I EI AI E I AI E IIAII E A 1 1 1 f P 0 1 1 u f P fI f II PI PII lI lI lII lII 2 2 2 2 1 2 1 u f P EII AII EII AII EIII AIII EIII AIII f II f III PII PIII 0 3 3 3 2 1 2 1 lII lII lIII lIII u f P f III PIII 4 4 4 2 2 EIII AIII EIII AIII 0 0 lIII lIII 19
Approximation Methods –Finite Element Method Example (cont): Step 5: Assembling to form systemequation Approach 2: Element connectivity table Element 1 Element 2 Element 3 k e K 1 1 2 3 ij IJ 2 2 3 4 local node global node index (i,j) (I,J) 20
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