Andere Kunden interessierten sich auch für
![Laser Damage in Calcium Fluoride]( "Laser Damage in Calcium Fluoride")
Laser Damage in Calcium Fluoride45,99 €![New Steady-state Cosmology and Criticism to Universal Big Bang]( "New Steady-state Cosmology and Criticism to Universal Big Bang")
New Steady-state Cosmology and Criticism to Universal Big Bang23,99 €![How To Simulate Solid State Devices, EFT & BJT]( "How To Simulate Solid State Devices, EFT & BJT")
How To Simulate Solid State Devices, EFT & BJT36,99 €![Application of perturbation theory to the finite size of the proton]( "Application of perturbation theory to the finite size of the proton")
Application of perturbation theory to the finite size of the proton26,99 €![Quantum Field Theory approaches to Early Universe Cosmology]( "Quantum Field Theory approaches to Early Universe Cosmology")
Quantum Field Theory approaches to Early Universe Cosmology42,99 €![Introduction to Physics for Remedial Program]( "Introduction to Physics for Remedial Program")
Introduction to Physics for Remedial Program55,99 €![Electronic Structures of Semiconductor Quantum Dots]( "Electronic Structures of Semiconductor Quantum Dots")
Electronic Structures of Semiconductor Quantum Dots44,99 €
In this work, we studied fatigue fracture and crack in composite aircraft. In which we studied airfoil NACA 2412 made of glass fiber.First, in the experimental part, experiments were carried out on two laminate plates(carbon/glass) with 8 plies, the first one controlled by ultrasonicmethode non destructive testing techniques (NDT) to detect cracks and also determine the mechanical caractérization. And other traction experience on both plates and have the results.Secondly , the simulation of airfoil NACA 2412 deduce displacement, deformation, stresses and strain ,7 modes shapes, and natural frequencies.