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151014s2016 enk ob 001 0 eng d |
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|a 925977975
|a 929521767
|a 1066631811
|a 1088958125
|a 1228588324
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|a 9780124171725
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|a 0124171729
|q (electronic bk.)
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|z 9780124171534
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|a (OCoLC)924207877
|z (OCoLC)925977975
|z (OCoLC)929521767
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|z (OCoLC)1088958125
|z (OCoLC)1228588324
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|a TA418.9.C6
|b W36 2016eb
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|a 620.1/18
|2 23
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|a Wang, Chun Hui
|c (Principal research scientist),
|e author.
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|a Bonded joints and repairs to composite airframe structures /
|c Chun H. Wang, Cong N. Duong.
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|a London :
|b Academic Press is an imprint of Elsevier,
|c [2016]
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| 300 |
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|a 1 online resource (x, 295 pages)
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| 336 |
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a Includes bibliographical references and index.
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|a Vendor-supplied metadata.
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|a Front Cover; Bonded Joints and Repairs to Composite Airframe Structures; Copyright; Contents; Preface; References; Part 1: Analysis and design; Chapter 1: Introduction and overview; 1.1. Aim of Book; 1.2. Criticality of Structure and Damage; 1.3. Types of Composite Repairs and Certification Criteria; 1.4. Overview of Repair Design and Analysis Process; 1.5. Effect of Load Attraction in Patch Design; 1.6. Effect of Taper and Scarf Ratios on Joint Design; 1.6.1. Safe-Life Approach; 1.6.2. Damage Tolerance Approach; 1.6.3. Stepped Repairs; 1.7. Summary; References; Chapter 2: Failure criteria
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|a 2.1. Introduction2.2. Adhesive Failure Criteria; 2.2.1. Failure Criteria for Brittle Adhesives; 2.2.2. Failure Criteria for Ductile Adhesives; 2.3. Composite Failure Criteria; 2.3.1. Intralamina Failure Criteria; 2.3.1.1. Maximum stress or strain failure criteria; 2.3.1.2. Tsai-Hill and Tsai-Wu failure criteria; 2.3.1.3. Hashin failure criteria; 2.3.1.4. Larc03 criteria; 2.3.2. Interlaminar Failure Criteria; 2.4. Summary; References; Chapter 3: Doubler joint analysis; 3.1. Introduction; 3.2. Untapered doublers and joints; 3.2.1. Two-Sided Doublers and Double Strap Joints
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|a 3.2.1.1. Elastic Analysis for Adhesive Shear3.2.1.2. Elastic-Plastic Analysis for Adhesive Shear; 3.2.1.3. Uncoupled Analysis of Adhesive Peel; 3.2.2. One-Sided Doublers and Single Strap Joints; 3.3. Tapered doublers and joints; 3.3.1. Solution for Nonlinear Moment Distribution Along the Joint; 3.3.2. Elastic Solution for Adhesive Peel and Shear; 3.3.2.1. Multisegment Method of Integration; 3.3.3. Elastic-Plastic Solution for Adhesive Peel and Shear; 3.3.4. Effect of Adherent Shear Deformation; 3.3.5. Numerical Examples; 3.4. Summary; References
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|a Chapter 4: Design of scarf and doubler-scarf joints4.1. Introduction; 4.2. Scarf joint of homogeneous adherends; 4.2.1. Constant-Angle Scarf; 4.2.2. Optimum Angle of Scarf Between Dissimilar Materials; 4.3. Composite scarf joint; 4.3.1. Identical Adherends with Constant-Angle Scarf; 4.3.2. Elasto-Plastic Stress Analysis of Scarf Joints; 4.4. Experiments and validation; 4.4.1. Room Temperature Dry Condition; 4.4.2. Hot Wet Condition; 4.5. Doubler-scarf joints; 4.6. Conclusions; References; Chapter 5: Disbond and damage tolerance analysis of doubler repairs; 5.1. Introduction
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|a 5.2. Analytical methods for delamination analysis5.2.1. VCCT by FE Method; 5.2.2. Crack Tip Element Approach; 5.2.2.1. Davidson's crack tip element approach; 5.2.2.2. Wang and Qiao crack tip element approach; 5.2.3. Cohesive Zone Model; 5.2.3.1. 1D cohesive zone model; 5.2.3.2. 2D cohesive zone model; 5.3. Analytical methods for disbond analysis; 5.4. Fatigue damage accumulation model for predicting interlaminar failure and disbond; 5.5. Summary; References; Chapter 6: Damage tolerance and fatigue durability of scarf joints; 6.1. Introduction; 6.2. Impact Damage of Scarf Joints and Repairs
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| 650 |
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|a Fibrous composites.
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| 650 |
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|a Airframes
|x Design and construction.
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| 650 |
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6 |
|a Composites �a fibres.
|0 (CaQQLa)201-0024427
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| 650 |
|
7 |
|a fibrous composite.
|2 aat
|0 (CStmoGRI)aat300189659
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| 650 |
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7 |
|a TECHNOLOGY & ENGINEERING
|x Engineering (General)
|2 bisacsh
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| 650 |
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|a TECHNOLOGY & ENGINEERING
|x Reference.
|2 bisacsh
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| 650 |
|
7 |
|a Airframes
|x Design and construction
|2 fast
|0 (OCoLC)fst00802914
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| 650 |
|
7 |
|a Fibrous composites
|2 fast
|0 (OCoLC)fst00923679
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| 700 |
1 |
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|a Duong, Cong N.,
|e author.
|
| 776 |
0 |
8 |
|i Print version:
|a Wang, Chun Hui.
|t Bonded Joints and Repairs to Composite Airframe Structures.
|d Saint Louis : Elsevier Science, �2015
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| 856 |
4 |
0 |
|u https://sciencedirect.uam.elogim.com/science/book/9780124171534
|z Texto completo
|
