High-Temperature Matrix Cracking, Opening and Closure in Ceramic-Matrix Composites

Longbiao Li

ISBN 10: 103263751X / ISBN 13: 9781032637518

Published by CRC Press, 2023

About this Item

nach der Bestellung gedruckt Neuware - Printed after ordering - Ceramic matrix composites (CMCs) can withstand higher temperatures, reduce cooling airflow, improve turbine efficiency, and greatly reduce structural mass compared to the high temperature alloys. This book focuses on the matrix first/multiple cracking, crack opening and closure behavior in CMCs at high temperatures.While conducting in situ experimental observations to analyze the damage mechanisms and failure modes, the author develops micromechanical damage models and constitutive models to predict the first matrix cracking stress, multiple matrix cracking density, matrix crack opening displacement, and cracking closure stress at high temperatures. The effects of composite's constituent properties, stress level, and ambient temperature on matrix cracking, opening, and closure are also discussed.This book will help material scientists and engineering designers to understand and master the matrix cracking and closure behavior of fiber-reinforced CMCs.

Seller Inventory # 9781032637518

Bibliographic Details

• Title: High-Temperature Matrix Cracking, Opening and Closure in Ceramic-Matrix Composites
• Publisher: CRC Press
• Publication Date: 2023
• Language: English
• ISBN 10: 103263751X
• ISBN 13: 9781032637518
• Binding: Buch
• Condition: Neu
• Dimensions: 240W x 161H x 12D millimeters 240 millimeters width by 161 millimeters height by 12 millimeters depth
• Weight: 385 grams

About this title

Synopsis

Ceramic matrix composites (CMCs) can withstand higher temperatures, reduce cooling airflow, improve turbine efficiency, and greatly reduce structural mass compared to the high temperature alloys. This book focuses on the matrix first/multiple cracking, crack opening and closure behavior in CMCs at high temperatures.

While conducting in situ experimental observations to analyze the damage mechanisms and failure modes, the author develops micromechanical damage models and constitutive models to predict the first matrix cracking stress, multiple matrix cracking density, matrix crack opening displacement, and cracking closure stress at high temperatures. The effects of composite’s constituent properties, stress level, and ambient temperature on matrix cracking, opening, and closure are also discussed.

This book will help material scientists and engineering designers to understand and master the matrix cracking and closure behavior of fiber-reinforced CMCs.

About the Author

Longbiao Li is a lecturer at College of Civil Aviation, Nanjing University of Aeronautics and Astronautics. Dr. Li’s research focuses on the vibration, fatigue, damage, fracture, reliability, safety and durability of aircraft and aero engines. In this research area, he is the first author of 204 SCI journal publications (59 JCR Q1), 11 monographs, 4 edited books, 4 textbooks, 3 book chapters, 33 Chinese patents, 2 US patents, 2 Chinese software copyrights, and more than 30 refereed conference proceedings. He has been involved in different projects related to structural damage, reliability, and airworthiness design for aircraft and aero engines, supported by the Natural Science Foundation of China, COMAC Company, and AECC Commercial Aircraft Engine Company.