Flávio Luiz de Silva Bussamra, Dr.
Associate Professor

(Professor Associado)

ITA - Divisão de Engenharia Aeronáutica
Aeronautical Engineering
Head of Department of Aeronautical Structures
Praça Marechal Eduardo Gomes, 50 - Vila das Acácias
CEP 12228-900 – São José dos Campos – SP – Brasil
 


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CONTACT


RESEARCH LINES


EDUCATION


TEACHING COURSES

Undergraduate level

 

EST-22 - Theory of Structures

Experimental stress analysis: electrical strain-gages and photo-elasticity. Work and energy principles. Analysis of bar structures. Force method. Rayleigh-Ritz method. Introduction to Finite Element Method: bars and plane elasticity. Bibliography: Allen, D. H. e Haisler, W. E. Introduction to aerospace structural analysis, New York, John Wiley, 1985; Dally, J. W. e Riley, W. F., Experimental stress analysis, 3ª ed., New York, McGraw-Hill, 1991; Assan, A.E., Método dos Elementos Finitos, Editora da Unicamp, 1999. 

EST-34 - Theory of Aircraft Structures
Introduction to aircraft structures: components and materials. Structural modelling by Finite Element Method. Plate theory of Kirchhoff. Torsion of bars: Saint-Venant theory and membrane analogy. Analysis of thin wall beams with open and closed sections. Structural constraint in thin wall beams. Shear lag. Wings and fuselages analysis.Joint analysis.
Bibliography: Megson, T. H. G., Aircraft structures for engineering students, 3a. ed., London, E. Arnold, 1999;. Bruhn, E. F., Analysis and design of flight vehicle structures, Cincinnati, Tri-Offset, 1973; Curtis, H., Fundamentals of aircraft structural analysis, New York, McGraw-Hill, 1997.

EST-50 -Structural Dynamics

Free and forced vibrations of SDOF linear systems. Free and forced vibrations of MDOF linear systems. Modal superposition. Direct integration methods for dynamic response. Free and forced vibrations of continuous systems. Introduction to random vibrations. Introduction to nonlinear systems. Finite element method in dynamics of structures.
Bibliography: Bismarck-Nasr, M. N., Structural dynamics in aeronautical engineering, Reston, Virginia, AIAA, 1999 AIAA Education Series); Clough, R. e Penzien, J., Dynamics of structures, 2ª ed., New York, McGraw-Hill College, 1993; Hagedorn, P., Oscilações não-lineares, São Paulo, Edgard Blucher Ltda, 1984.

PRJ-45 - Design and Construction of Airmodels
 


Graduate level

AE-256 - Numerical methods in solid mechanics
Linear algebra. Polynomial interpolation. Numerical integration. Direct and iterative methods for of equilibrium equations in static analysis. Direct integration methods in dynamic analysis. Eigensystems: transformation methods, vector iteration method, Subspace iteration method.
Bibliography: Bathe, K.-J., Finite element procedures, Prentice Hall, New Jersey, 1996; Burden, R.L. e Faires, J.D., Análise numérica, ABPDEA, Thomson, São Paulo, 2003; Yang, W.Y., Cao, W., Chang, T.-S. e Morris, J., Applied numerical methods using Matlab, Wiley, New York, 2005.

AE-225 - Structural Dynamics I

D'Alambert and Hamilton Principles. Lagrange equations. Analysis of single and multiple degree of freedom systems: free and forced vibrations. Modal superposition technique. Vibration of continuum systems. Rayleigh-Ritz Method. Finite Element Method. Bibliography: Bismarck-Nasr, M.N., Structural dynamics in aeronautical engineering, AIAA Education Series, Reston, Virginia, 1999; Craig, R.R., Structural dynamics: an introduction to computer methods, John Wiley & Sons, 1981; Meirovitch, L., Elements of vibration analysis, 2a. ed., McGraw-Hill, New York, 1986.

 

AE-245 - Finite Elements I

Basis of the finite element method. Finite elements in elastostatics. Element formulation based on the weak form and principle of total potential energy. Isoparametric elements, mixed formulation. Introduction to calculus of variations. Beam and plate elements. Shear locking effect. Bibliography: Hughes TJR, The Finite Element Method, Prentice-Hall, Englewood Cliffs, New Jersey, 1987; Strang G, Fix GJ, An Analysis of the Finite Element Method, Prentice-Hall, Englewood Cliffs, NJ, 1973; Weinstock R, Calculus of Variations with Applications to Physics and Engineering, McGraw-Hill, New York, 1952.


AE-701 - Aircraft Structures Analysis


 


CURRICULUM

 

Link to: Lattes Curriculum
 


MATERIAL

   AE-245 - Lista 1