Handbook of materials failure analysis with case studies from the aerospace and automotive industries

Handbook of Materials Failure Analysis: With Case Studies from the Aerospace and Automotive Industries provides a thorough understanding of the reasons materials fail in certain situations, covering important scenarios, including material defects, mechanical failure as a result of improper design, c...

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Bibliographic Details
Other Authors: Makhlouf, Abdel Salam Hamdy, (Editor), Aliofkhazraei, Mahmood, (Editor)
Format: eBook
Language: English
Published: Oxford, UK : Butterworth-Heinemann is an imprint of Elsevier, 2015.
Subjects:
ISBN: 9780128011775
0128011777
9780128009505
0128009500
Physical Description: 1 online resource

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035 |a (OCoLC)919719550  |z (OCoLC)919872020  |z (OCoLC)920019349  |z (OCoLC)922283379  |z (OCoLC)963185149 
245 0 0 |a Handbook of materials failure analysis with case studies from the aerospace and automotive industries /  |c edited by Abdel Salam Hamdy Makhlouf, Mahmood Aliofkhazraei. 
264 1 |a Oxford, UK :  |b Butterworth-Heinemann is an imprint of Elsevier,  |c 2015. 
264 4 |c ©2016 
300 |a 1 online resource 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
500 |a Includes index. 
505 0 |a Front Cover; Handbook of Materials Failure Analysis With Case Studies from the Aerospace and Automotive Industries; Copyright; Contents; Contributors; Preface; Part 1: Failure analysis in aircraft and aerospace structures; Chapter 1: Strategies for static failure analysis on aerospace structures; 1. Introduction; 2. Delamination Growth in Composites; 2.1. VCCT Fundamentals; 2.2. Experimental Benchmark and FEM Simulation; 2.3. FEMs Comparison; 2.4. Delamination Growth Tool; 2.5. Correlation Between FEM Simulations and Tests; 2.6. Mesh Size Effects. 
505 8 |a 2.7. Comparison of Mixed-Mode Failure Criteria2.8. Conclusion and Further Work in Delamination Growth Analysis; 3. Debonding Onset and Growth; 3.1. DCB Coupon: Mode I Interlaminar Fracture Toughness Test; 3.2. FE Modeling; 3.3. CZ Fundamentals; 3.4. Mesh Dependency; 3.5. Experimental Results; 3.6. Correlation FEM Simulation-Tests; 3.7. Conclusion and Future Work in Debonding Analysis; 4. Crack Growth in Metallic Structures; 4.1. CTOA Criterion-Experimental Obtaining of CTOAC; 4.2. Crack Growth Tool; 4.3. Benchmarks Description; 4.4. FEM Modeling; 4.5. Correlation Simulations-Tests. 
505 8 |a 4.6. Crack Growth in Metallic Structures-Conclusion and Future WorkReferences; Chapter 2: Strategies for dynamic failure analysis on aerospace structures; 1. Introduction; 2. Land Incidents; Low-Velocity Impacts; 2.1. FEM Modeling and Analysis; 2.2. Conclusion and Recommendations; 3. Land Incidents; Frangibility of Airport Structures; 3.1. Design to be Analyzed; 3.2. Numerical Analysis Tool Used in Impact Problems; 3.3. Model Correlation with Lateral Loading Test; 3.4. Mechanical Properties and Failure Criterion Validation; 3.5. Frangibility Simulation Results; 4. Flight Incidents. 
505 8 |a Blade Loss of a Transport Aircraft4.1. Blade-Loss Phenomenon; 4.2. Description of the Models; 4.3. FEM Model and Simplified Model; 4.4. Analysis Considerations, Implicit and Explicit Method, Time Step; 4.5. Loads and Boundary Conditions; 4.6. Load Cases Analyzed; 4.7. Results; 4.8. Conclusion; 5. Conclusion; Acknowledgments; References; Chapter 3: The evolution of failure analysis at NASAs Kennedy Space Center and lessons learned; 1. Introduction; 2. Long-Duration Space Operations; 2.1. Skylab; 2.2. International Space Station; 3. Failure in LEO: The Solar Alpha Rotary Joint. 
505 8 |a 3.1. STS-117 Mission Overview3.2. SARJ Hardware Overview; 3.3. STS-117 Mission Details; 4. The Problem; 4.1. Troubleshooting During the STS-120 Mission; 4.2. Initial KSC SARJ Investigation; 4.3. NASA SARJ Investigation; 4.4. Expedition 16 Sample Analysis; 4.5. Postanalysis On-orbit Inspection; 4.6. The Repair on STS-126, November 2008; 4.7. What About the Port-SARJ?; 5. Conclusion; References; Chapter 4: Fleet impact resulting from a space shuttle Columbia main engine controller wire failure during Mission STS-93; 1. Space Shuttle Columbia Wiring Hardware Overview; 2. Investigation. 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
520 |a Handbook of Materials Failure Analysis: With Case Studies from the Aerospace and Automotive Industries provides a thorough understanding of the reasons materials fail in certain situations, covering important scenarios, including material defects, mechanical failure as a result of improper design, corrosion, surface fracture, and other environmental causes. The book begins with a general overview of materials failure analysis and its importance, and then logically proceeds from a discussion of the failure analysis process, types of failure analysis, and specific tools and techniques, to c. 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Materials  |x Fatigue  |v Handbooks, manuals, etc. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
700 1 |a Makhlouf, Abdel Salam Hamdy,  |e editor. 
700 1 |a Aliofkhazraei, Mahmood,  |e editor. 
776 0 8 |i Print version:  |a Makhlouf, Abdel Salam Hamdy.  |t Handbook of Materials Failure Analysis with Case Studies from the Aerospace and Automotive Industries : With case studies from the aerospace, chemical, and oil and gas industries.  |d Burlington : Elsevier Science, ©2015  |z 9780128009505 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kp0M7W3TI4/handbook-of-materials?kpromoter=marc  |y Full text