Titlebook: Advances in Mechanical Engineering and Mechanics III; Selected Papers from Tarak Bouraoui,Naoufel Ben Moussa,Fathi Djemal Conference procee

Adrenal-Glands

Zusammenfassende Berechnung der Traglagerens by means of compressive residual stress. The present paper will examine the effect of coverage rate on a leading edge of turbine blades. In this context, a 3D model of thin leading-edge parts made of Ti-6Al-4V is performed with ABAQUS software. The objective of this simulation involves the predi

admission

Unvollkommene und vollkommene SchmierungAl-4V alloy under different ballistic tests is made. We investigates the effects of target thickness, projectile nose shapes and strike velocities for an orthogonal perforation on the projectile velocity and its residual one. Johnson-Cook constitutive law and its associated damage model are used to

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allude

CT-angiography

978-3-031-70427-7The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl