Advances In Fatigue And Fracture Mechanics Analyses For Metallic Aircraft Structures

Download Advances In Fatigue And Fracture Mechanics Analyses For Metallic Aircraft Structures full books in PDF, epub, and Kindle. Read online Advances In Fatigue And Fracture Mechanics Analyses For Metallic Aircraft Structures ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!

Advances in Fatigue and Fracture Mechanics Analyses for Metallic Aircraft Structures

Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
ISBN 13 : 9781723796654
Total Pages : 46 pages
Book Rating : 4.7/5 (966 download)

DOWNLOAD NOW!

Book Synopsis Advances in Fatigue and Fracture Mechanics Analyses for Metallic Aircraft Structures by : National Aeronautics and Space Adm Nasa

Download or read book Advances in Fatigue and Fracture Mechanics Analyses for Metallic Aircraft Structures written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-18 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper reviews some of the advances that have been made in stress analyses of cracked aircraft components, in the understanding of the fatigue and fatigue-crack growth process, and in the prediction of residual strength of complex aircraft structures with widespread fatigue damage. Finite-element analyses of cracked metallic structures are now used to determine accurate stress-intensity factors for cracks at structural details. Observations of small-crack behavior at open and rivet-loaded holes and the development of small-crack theory has lead to the prediction of stress-life behavior for components with stress concentrations under aircraft spectrum loading. Fatigue-crack growth under simulated aircraft spectra can now be predicted with the crack-closure concept. Residual strength of cracked panels with severe out-of-plane deformations (buckling) in the presence of stiffeners and multiple-site damage can be predicted with advanced elastic-plastic finite-element analyses and the critical crack-tip-opening angle (CTOA) fracture criterion. These advances are helping to assure continued safety of aircraft structures.Newman, J. C., Jr.Langley Research CenterAIRCRAFT STRUCTURES; CRACKS; FINITE ELEMENT METHOD; FRACTURE MECHANICS; STRESS ANALYSIS; METALS; CRACK PROPAGATION; METAL FATIGUE; STRESS INTENSITY FACTORS; RESIDUAL STRENGTH; CRACK CLOSURE; DAMAGE; STRESS CONCENTRATION; RIVETED JOINTS; PLASTIC PROPERTIES

Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components

Author : Russell Wanhill
Publisher :
ISBN 13 : 9789402416749
Total Pages : 99 pages
Book Rating : 4.4/5 (167 download)

DOWNLOAD NOW!

Book Synopsis Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components by : Russell Wanhill

Download or read book Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components written by Russell Wanhill and published by . This book was released on 2019 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book provides a concise discussion of fatigue crack growth (FCG) failure and lifing analysis methods for metallic aircraft structures and components. After a reasonably concise historical review, surveys are made of (i) the importance of fatigue for aircraft structural failures and the sources of fatigue nucleation and cracking, (ii) contemporary FCG lifing methods, and (iii) the Quantitative Fractography (QF) required for determining the actual FCG behaviour. These surveys are followed by the main part of the book, which is a discussion, using case histories, of the applicabilities of Linear Elastic Fracture Mechanics (LEFM) and non-LEFM methods for analysing service fatigue failures and full- and sub-scale test results. This discussion is derived primarily from the experiences of the Defence Science and Technology Group in Melbourne, Australia, and the Netherlands Aerospace Centre, Marknesse, the Netherlands.

Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components

Author : Russell Wanhill
Publisher : Springer
ISBN 13 : 9402416757
Total Pages : 99 pages
Book Rating : 4.4/5 (24 download)

DOWNLOAD NOW!

Book Synopsis Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components by : Russell Wanhill

Download or read book Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components written by Russell Wanhill and published by Springer. This book was released on 2019-02-19 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book provides a concise discussion of fatigue crack growth (FCG) failure and lifing analysis methods for metallic aircraft structures and components. After a reasonably concise historical review, surveys are made of (i) the importance of fatigue for aircraft structural failures and the sources of fatigue nucleation and cracking, (ii) contemporary FCG lifing methods, and (iii) the Quantitative Fractography (QF) required for determining the actual FCG behaviour. These surveys are followed by the main part of the book, which is a discussion, using case histories, of the applicabilities of Linear Elastic Fracture Mechanics (LEFM) and non-LEFM methods for analysing service fatigue failures and full- and sub-scale test results. This discussion is derived primarily from the experiences of the Defence Science and Technology Group in Melbourne, Australia, and the Netherlands Aerospace Centre, Marknesse, the Netherlands.

Advances in Fatigue and Fracture Mechanics Analyses for Metallic Aircraft Structures

Author : J. C. Newman (Jr)
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!

Book Synopsis Advances in Fatigue and Fracture Mechanics Analyses for Metallic Aircraft Structures by : J. C. Newman (Jr)

Download or read book Advances in Fatigue and Fracture Mechanics Analyses for Metallic Aircraft Structures written by J. C. Newman (Jr) and published by . This book was released on 2000 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Damage Tolerance of Metallic Aircraft Structures

Author : Sérgio M. O. Tavares
Publisher : Springer
ISBN 13 : 3319701908
Total Pages : 106 pages
Book Rating : 4.3/5 (197 download)

DOWNLOAD NOW!

Book Synopsis Damage Tolerance of Metallic Aircraft Structures by : Sérgio M. O. Tavares

Download or read book Damage Tolerance of Metallic Aircraft Structures written by Sérgio M. O. Tavares and published by Springer. This book was released on 2018-08-06 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book provides a state-of-the-art review of the fail-safe and damage tolerance approaches, allowing weight savings and increasing aircraft reliability and structural integrity. The application of the damage tolerance approach requires extensive know-how of the fatigue and fracture properties, corrosion strength, potential failure modes and non-destructive inspection techniques, particularly minimum detectable defect and inspection intervals. In parallel, engineering practice involving damage tolerance requires numerical techniques for stress analysis of cracked structures. These evolved from basic mode I evaluations using rough finite element approaches, to current 3D modeling based on energetic approaches as the VCCT, or simulation of joining processes. This book provides a concise introduction to this subject.

Design of Fatigue and Fracture Resistant Structures

Author : P. R. Abelkis
Publisher : ASTM International
ISBN 13 : 9780803107144
Total Pages : 500 pages
Book Rating : 4.1/5 (71 download)

DOWNLOAD NOW!

Book Synopsis Design of Fatigue and Fracture Resistant Structures by : P. R. Abelkis

Download or read book Design of Fatigue and Fracture Resistant Structures written by P. R. Abelkis and published by ASTM International. This book was released on 1982 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Damage Tolerance of Metallic Structures

Author : J. B. Chang
Publisher : ASTM International
ISBN 13 : 9780803104075
Total Pages : 168 pages
Book Rating : 4.1/5 (4 download)

DOWNLOAD NOW!

Book Synopsis Damage Tolerance of Metallic Structures by : J. B. Chang

Download or read book Damage Tolerance of Metallic Structures written by J. B. Chang and published by ASTM International. This book was released on 1984 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fracture Control Procedures for Aircraft Structural Integrity

Author : Howard A. Wood
Publisher :
ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!

Book Synopsis Fracture Control Procedures for Aircraft Structural Integrity by : Howard A. Wood

Download or read book Fracture Control Procedures for Aircraft Structural Integrity written by Howard A. Wood and published by . This book was released on 1971 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report reviews the application of applied fracture mechanics in the design, analysis and qualification of aircraft structural systems. Recent service experiences are cited. Current trends in high strength materials application are reviewed with particular emphasis on the manner in which fracture toughness and structural efficiency may affect the material selection process. General fracture control procedures are reviewed in depth with specific reference to the impact of inspectability, structural arrangement and material on proposed analysis requirements for safe crack growth. The relative impact on allowable design stress is indicated by example. Design criteria, material and analysis requirements for implementation of fracture control procedures are reviewed together with limitation in current available data techniques. A summary of items which require further study and attention is presented.

Handbook of Materials Failure Analysis with Case Studies from the Aerospace and Automotive Industries

Author : Abdel Salam Hamdy Makhlouf
Publisher : Butterworth-Heinemann
ISBN 13 : 0128011777
Total Pages : 524 pages
Book Rating : 4.1/5 (28 download)

DOWNLOAD NOW!

Book Synopsis Handbook of Materials Failure Analysis with Case Studies from the Aerospace and Automotive Industries by : Abdel Salam Hamdy Makhlouf

Download or read book Handbook of Materials Failure Analysis with Case Studies from the Aerospace and Automotive Industries written by Abdel Salam Hamdy Makhlouf and published by Butterworth-Heinemann. This book was released on 2015-09-01 with total page 524 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 chapters on analysis of materials failure from various causes. Later chapters feature a selection of newer examples of failure analysis cases in such strategic industrial sectors as aerospace, oil & gas, and chemicals. Covers the most common types of materials failure, analysis, and possible solutions Provides the most up-to-date and balanced coverage of failure analysis, combining foundational knowledge, current research on the latest developments, and innovations in the field Ideal accompaniment for those interested in materials forensic investigation, failure of materials, static failure analysis, dynamic failure analysis, fatigue life prediction, rotorcraft, failure prediction, fatigue crack propagation, bevel pinion failure, gasketless flange, thermal barrier coatings Presents compelling new case studies from key industries to demonstrate concepts Highlights the role of site conditions, operating conditions at the time of failure, history of equipment and its operation, corrosion product sampling, metallurgical and electrochemical factors, and morphology of failure

Fatigue of Aircraft Structures

Author : United States. Naval Air Systems Command
Publisher :
ISBN 13 :
Total Pages : 360 pages
Book Rating : 4.F/5 ( download)

DOWNLOAD NOW!

Book Synopsis Fatigue of Aircraft Structures by : United States. Naval Air Systems Command

Download or read book Fatigue of Aircraft Structures written by United States. Naval Air Systems Command and published by . This book was released on 1966 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Service Fatigue Loads Monitoring, Simulation, Analysis - Stp 671

Author : P. R. Abelkis
Publisher : ASTM International
ISBN 13 : 9780803107212
Total Pages : 298 pages
Book Rating : 4.1/5 (72 download)

DOWNLOAD NOW!

Book Synopsis Service Fatigue Loads Monitoring, Simulation, Analysis - Stp 671 by : P. R. Abelkis

Download or read book Service Fatigue Loads Monitoring, Simulation, Analysis - Stp 671 written by P. R. Abelkis and published by ASTM International. This book was released on 1979 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Handbook of Structural Life Assessment

Author : Raouf A. Ibrahim
Publisher : John Wiley & Sons
ISBN 13 : 1119135486
Total Pages : 1016 pages
Book Rating : 4.1/5 (191 download)

DOWNLOAD NOW!

Book Synopsis Handbook of Structural Life Assessment by : Raouf A. Ibrahim

Download or read book Handbook of Structural Life Assessment written by Raouf A. Ibrahim and published by John Wiley & Sons. This book was released on 2017-03-29 with total page 1016 pages. Available in PDF, EPUB and Kindle. Book excerpt: This important, self-contained reference deals with structural life assessment (SLA) and structural health monitoring (SHM) in a combined form. SLA periodically evaluates the state and condition of a structural system and provides recommendations for possible maintenance actions or the end of structural service life. It is a diversified field and relies on the theories of fracture mechanics, fatigue damage process, and reliability theory. For common structures, their life assessment is not only governed by the theory of fracture mechanics and fatigue damage process, but by other factors such as corrosion, grounding, and sudden collision. On the other hand, SHM deals with the detection, prediction, and location of crack development online. Both SLA and SHM are combined in a unified and coherent treatment.

USAF Damage Tolerant Design Handbook

Author :
Publisher :
ISBN 13 :
Total Pages : 636 pages
Book Rating : 4.E/5 ( download)

DOWNLOAD NOW!

Book Synopsis USAF Damage Tolerant Design Handbook by :

Download or read book USAF Damage Tolerant Design Handbook written by and published by . This book was released on 1984 with total page 636 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Proceedings of the 9th International Symposium on Superalloy 718 & Derivatives: Energy, Aerospace, and Industrial Applications

Author : Eric Ott
Publisher : Springer
ISBN 13 : 3319894803
Total Pages : 1118 pages
Book Rating : 4.3/5 (198 download)

DOWNLOAD NOW!

Book Synopsis Proceedings of the 9th International Symposium on Superalloy 718 & Derivatives: Energy, Aerospace, and Industrial Applications by : Eric Ott

Download or read book Proceedings of the 9th International Symposium on Superalloy 718 & Derivatives: Energy, Aerospace, and Industrial Applications written by Eric Ott and published by Springer. This book was released on 2018-05-12 with total page 1118 pages. Available in PDF, EPUB and Kindle. Book excerpt: This technical meeting will focus on Alloy 718 and Superalloys in this class relative to alloy and process development, production, product applications, trends and the development of advanced modeling tools. The symposium provides an opportunity for authors to present technical advancements relative to a broad spectrum of areas while assessing their impact on related fields associated with this critical alloy group. There are continuing innovations relative to these alloys as well as novel processing techniques which continue to extend applications in very challenging environments ranging from corrosion resistance in the deep sea to high-stressed space applications.

FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance

Author : Charles E. Harris
Publisher :
ISBN 13 :
Total Pages : 520 pages
Book Rating : 4.:/5 (317 download)

DOWNLOAD NOW!

Book Synopsis FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance by : Charles E. Harris

Download or read book FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance written by Charles E. Harris and published by . This book was released on 1994 with total page 520 pages. Available in PDF, EPUB and Kindle. Book excerpt:

USAF Damage Tolerant Design Handbook

Author :
Publisher :
ISBN 13 :
Total Pages : 752 pages
Book Rating : 4.E/5 ( download)

DOWNLOAD NOW!

Book Synopsis USAF Damage Tolerant Design Handbook by :

Download or read book USAF Damage Tolerant Design Handbook written by and published by . This book was released on 1984 with total page 752 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Durability Methods Development

Author : S. D. Manning
Publisher :
ISBN 13 :
Total Pages : 228 pages
Book Rating : 4.3/5 (91 download)

DOWNLOAD NOW!

Book Synopsis Durability Methods Development by : S. D. Manning

Download or read book Durability Methods Development written by S. D. Manning and published by . This book was released on 1979 with total page 228 pages. Available in PDF, EPUB and Kindle. Book excerpt: A summary is presented of an analytical methodology developed to meet USAF durability requirements. Details are given in four companion volumes. Analytical approaches that are currently used or have potential to be used to determine economic life are surveyed. Results of a structural survey of durability problems experienced at USAF ALC's are summarized. Durability critical parts criteria and economic life criteria are discussed. An analytical method to determine the crack population in a structure as a function of service time is presented. Fastener-hole cracking is the basic form of damage analyzed. Representations of initial quality and growth of small cracks are discussed. The effect of inspection and repair on the distribution of cracks is included.