Imagen del editor

Computational Modeling of Delamination in Aircraft Hybrid Laminates

Neelambaran Karapurath

0 valoraciones por Goodreads
ISBN 10: 3846541923 / ISBN 13: 9783846541920
Editorial: LAP Lambert Academic Publishing
Nuevos Condición: New Encuadernación de tapa blanda
Librería: BuySomeBooks (Las Vegas, NV, Estados Unidos de America)

Librería en AbeBooks desde: 21 de mayo de 2012

Cantidad: > 20

Comprar nuevo
Precio recomendado: 63.00
Precio: EUR 83,31 Convertir moneda
Gastos de envío: EUR 3,31 A Estados Unidos de America Destinos, gastos y plazos de envío
Añadir al carrito

Descripción

Paperback. 104 pages. Dimensions: 8.7in. x 5.9in. x 0.2in.Hybrid laminates and advanced composites represent the third generation of aerospace materials. Aircraft hybrid laminates display several desirable characteristics but are susceptible to delamination. The technical focus of this work was to simulate delamination in GLARE laminates subjected to Mode-I loading. The report aims to introduce delamination growth modelled as crack propagation through the resin rich adhesive layer. This goal was accomplished using an X-FEM crack growth model in Abacus FEA software. Mode-I loading was simulated based on DCB test according to ASTM standards. This monograph contains step by step instructions to model a typical test specimen, simulate a total delamination growth of 30 mm including post processing steps required to obtain load-displacement plots. The approach was validated by comparing the test results to experimental results and cohesive zone model data available in the literature. Unlike the CZM approach this model can be extended to simulate migration of delamination across the laminae. This item ships from multiple locations. Your book may arrive from Roseburg,OR, La Vergne,TN. N° de ref. de la librería 9783846541920

Hacer una pregunta a la librería

Detalles bibliográficos

Título: Computational Modeling of Delamination in ...

Editorial: LAP Lambert Academic Publishing

Encuadernación: Paperback

Condición del libro:New

Tipo de libro: Paperback

Acerca de

Sinopsis:

Hybrid laminates and advanced composites represent the third generation of aerospace materials. Aircraft hybrid laminates display several desirable characteristics but are susceptible to delamination. The technical focus of this work was to simulate delamination in GLARE laminates subjected to Mode-I loading.The report aims to introduce delamination growth modelled as crack propagation through the resin rich adhesive layer.This goal was accomplished using an X-FEM crack growth model in Abacus FEA software. Mode-I loading was simulated based on DCB test according to ASTM standards. This monograph contains step by step instructions to model a typical test specimen, simulate a total delamination growth of 30 mm including post processing steps required to obtain load-displacement plots. The approach was validated by comparing the test results to experimental results and cohesive zone model data available in the literature. Unlike the CZM approach this model can be extended to simulate migration of delamination across the laminae.

About the Author:

Neelambaran Karapurath has a Bachelors Degree in Aeronautics,a Bachelors Degree in Applied Information Technology and an Advanced diploma in Software Engineering.He has obtained a Masters Degree in Advanced Engineering from Sheffield Hallam University,U.K in 2011. He has worked in Materials and Engineering Research Institute,U.K.

"Sobre este título" puede pertenecer a otra edición de este libro.

Descripción de la librería

BuySomeBooks is great place to get your books online. With over eight million titles available we're sure to have what you're looking for. Despite having a large selection of new books available for immediate shipment and excellent customer service, people still tell us they prefer us because of our prices.

Ver la página web de la librería

Condiciones de venta:

We guarantee the condition of every book as it's described on the Abebooks web
sites. If you're dissatisfied with your purchase (Incorrect Book/Not as
Described/Damaged) or if the order hasn't arrived, you're eligible for a refund
within 30 days of the estimated delivery date. If you've changed your mind about a book that you've ordered, please use the Ask bookseller a question link to contact us and we'll respond within 2 business days.

BuySomeBooks is operated by Drive-On-In, Inc., a Nevada co...

Más información
Condiciones de envío:

Orders usually ship within 1-2 business days. Books are shipped from multiple locations so your order may arrive from Las Vegas,NV, Roseburg,OR, La Vergne,TN, Momence,IL, or Commerce,GA.

Todos los libros de esta librería

Métodos de pago
aceptados por la librería

Visa Mastercard American Express Carte Bleue