The purpose of this book is to illustrate step by step the design of the Composite Wing Structure of the external wing for an Unmanned Aerial Vehicle- UAV. The design is conducted using software tools for Finite Element Analysis, such as, NASTRAN and ANSYS to find the structural integrity limits for composite materials and fittings. Data for this study were obtained from AEROTECH Research Group at Universidad de San Buenaventura, Bogota, Colombia. Finite Element Methods are used in order to evaluate the static strength, maximum stresses and buckling behavior of composite structures. Sections, such as spars, webs and caps,.
Structural Design of a Composite Wing Structure: Analysis of an Unmanned Aerial Vehicle book
Structural Design of a Composite Wing Structure: Analysis of an Unmanned Aerial Vehicle reviews
Structural Design of a Composite Wing Structure: Analysis of an Unmanned Aerial Vehicle free ebook pdf epub
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