Lampeas George
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Lampeas George
Academic position: Professor
Laboratory member: Laboratory of Technology and Strength of Materials
Studies: 1989: Diploma in Mechanical & Aeronautics Engineering Dept, Univ. of Patras, 1995: Ph.D. Mechanical & Aeronautics Engineering Dept, Univ. of Patras; Thesis title:’Stress, stability and vibration analysis of composite plates by semi-analytical method’.
Professional Activities: 1989-1995: Post-graduate student of the Laboratory of Technology & Strength of Materials, Mechanical & Aeronautics Engineering Dept., Univ. of Patras, doctoral thesis in the field of stress analysis of light weight structures, 1991-1992: Scientific collaboration with the Ιnstitut fuer Leichtbau of RWTH Aachen-Germany, in the frame of a bilateral scientific programme, 1993-1995: Scientific collaboration at Dornier Luftfahrt A.G. in Friedrischafen-Germany, 1996-1999: Scientific collaboration with the Institute of Structures & Advanced Materials, Patras, 1999-2003: Research & Production Engineer at ELVAL S.A., 2003-today:Assistant Professor, Mechanical & Aeronautics Engineering Dept., Univ. of Patras.
Participation in the European Funded Research Projects Participation in 31 European Funded Research Projects in 9 of them as scientific responsible for Univ. Patras
Publications: More than 40 publications in scientific International Journals. More than 12 publications/presentations in scientific International Conferences, Publication in International Books: 3 publications in international books
Google Scholar: Lampeas George
Courses
Strength of Materials II
Description Beam bending: Stress analysis, Skew loading, Secondary moments of inertia, principal axes, deflection line, Double integration method, Curvature surfaces method, Castigliano method, Mohr...
Introduction to Aeronautical Materials
Description Material selection for lightweight structures – Aeronautical materials – Aluminum – Aluminum alloys (effect of alloying elements on the mechanical behavior, intermetallic phases,...
Special Topics in the Analysis of Aircraft Stuctures
COURSE CONTENT Stress and strain analysis of statically indeterminate multi-cell beams, basic concepts of fracture mechanics and their application in structural integrity. Certification and...
Analysis of Aerospace Structures
COURSE CONTENT The lightweight design philosophy and the application of strength of materials principles in lightweight design – Design principles. Analysis of thin-walled members...
Aeronautical Materials
Course Content Material selection for lightweight structures – Aeronautical materials – Aluminum – Aluminum alloys (effect of alloying elements on the mechanical behavior, intermetallic...
Light Structures
COURSE CONTENT The lightweight design philosophy and the application of strength of materials principles in lightweight design – Design principles. Analysis of thin-walled members...
Advanced Strength of Materials
COURSE CONTENT High thickness pipes under internal / external pressure. Limit tube strength under internal pressure, composite tubes. Beam analysis in elastic subsoil, applications...
Damage Tolerance Design
COURSE CONTENT Definitions, basic considerations, non-uniform loading conditions, characteristic dimensions, degradation of strength and stiffness, general description of the design methodology of damage tolerance....
Fracture Mechanics & Structural Integrity
COURSE CONTENT Fracture phenomena. Linear Mechanics of Fractures – Griffith Theory and Failure Criterion. The concept of stress intensity factors and methods for their...