β Scribed by Sook-Ying Ho
No coin nor oath required. For personal study only.
This book deals with structural failure (induced by mechanical, aerodynamic, acoustic and aero-thermal, loads, etc.) of modern aerospace vehicles, in particular high-speed aircraft, solid propellant rocket systems and hypersonic flight vehicles, where structural integrity, failure prediction and service life assessment are particularly challenging, due to the increasingly more demanding mission requirements and the use of non-traditional materials, such as non-metallic composites, in their construction. Prediction of the complex loading environment seen in high-speed operation and constitutive / fracture models which can adequately describe the non-linear behaviour exhibited by advanced alloys and composite materials are critical in analyzing the non-linear structural response of modern aerospace vehicles and structures. The state-of-the-art of the different structural integrity assessment and prediction methodologies (including non-destructive structural health monitoring techniques) used for the structural design, service life assessment and failure analysis of the different types of aerospace vehicles are presented. The chapters are written by experts from aerospace / defence research organizations and academia in the fields of solid mechanics, and structural mechanics and dynamics of aircraft, rocket and hypersonic systems. The book will serve as a useful reference document containing specialist knowledge on appropriate prediction methodologies for a given circumstance and experimental data acquired from multi-national collaborative programs. Read more...
01 Title.pdf......Page 1
02 Cover Page......Page 2
04 eBooks End User License Agreement-Website......Page 3
05 Content......Page 4
06 FOREWORD by Dr CT Liu......Page 5
07 Preface......Page 6
08 List of Contributors......Page 8
09 Nomenculture......Page 10
10 chapter 1 Fatigue life assessment paper V2a......Page 15
11 chapter 2 Generic design procedures for the repair of acoustically damaged panels Final a2......Page 32
12 chapter 3 aerothermostructural analysis_j......Page 68
13 chapter 4 Ebook-Zhuang20100202b......Page 99
14 chapter 5 Fracture Andrei and John 15a......Page 110
15 chapter 6 NDE solid rocket3......Page 147
16 chapter 7 solid rocket SIA5a......Page 170
17 INDEX......Page 192
Π’ΡΠ°Π½ΡΠΏΠΎΡΡ;ΠΡΡΠΎΠΊΠΎΡΠΌΠΈΡΠ΅ΡΠΊΠ°Ρ ΡΠ΅Ρ Π½ΠΈΠΊΠ°;
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