Author: American Society for Testing and Materials
Publisher: ASTM International
ISBN:
Category : Airframes
Languages : en
Pages : 260
Book Description
A Note on Helicopter Rotor-blade Fatigue-crack Propagation Rates Under Equivalent-lifetime Fatigue Loadings
Author: John F. Ward
Publisher:
ISBN:
Category : Loads (Mechanics)
Languages : en
Pages : 14
Book Description
Publisher:
ISBN:
Category : Loads (Mechanics)
Languages : en
Pages : 14
Book Description
Damage Tolerance in Aircraft Structures
Author: American Society for Testing and Materials
Publisher: ASTM International
ISBN:
Category : Airframes
Languages : en
Pages : 260
Book Description
Publisher: ASTM International
ISBN:
Category : Airframes
Languages : en
Pages : 260
Book Description
NASA Technical Note
Handbook of Case Histories in Failure Analysis, Volume 2
Author: Khlefa Alarbe Esaklul
Publisher: ASM International
ISBN: 9780871704955
Category : Technology & Engineering
Languages : en
Pages : 608
Book Description
Presents more than 120 expert failure analysis case histories from industries including automotive, aerospace, utilities, oil and gas, petrochemical, biomedical, ground transportation, off-highway vehicles, and more. Volume 2 builds on the tremendous acceptance of Volume 1 by the failure analysis community. The two volumes can also be purchased as a set for a special discounted price. Learn how others have investigated and solved failures in various industries involving a wide range of failure modes, materials, and analysis techniques.
Publisher: ASM International
ISBN: 9780871704955
Category : Technology & Engineering
Languages : en
Pages : 608
Book Description
Presents more than 120 expert failure analysis case histories from industries including automotive, aerospace, utilities, oil and gas, petrochemical, biomedical, ground transportation, off-highway vehicles, and more. Volume 2 builds on the tremendous acceptance of Volume 1 by the failure analysis community. The two volumes can also be purchased as a set for a special discounted price. Learn how others have investigated and solved failures in various industries involving a wide range of failure modes, materials, and analysis techniques.
Fatigue Crack Growth Failure and Lifing Analyses for Metallic Aircraft Structures and Components
Author: Russell Wanhill
Publisher: Springer
ISBN: 9402416757
Category : Technology & Engineering
Languages : en
Pages : 104
Book Description
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.
Publisher: Springer
ISBN: 9402416757
Category : Technology & Engineering
Languages : en
Pages : 104
Book Description
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.
Crack Propagation
Author: United States. Federal Aviation Agency. Administrative Services Division. Library Branch
Publisher:
ISBN:
Category : Metals
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Metals
Languages : en
Pages : 66
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 652
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 652
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Army R, D & A.
Army RD & A.
Damage Tolerance in Aircraft Structures
Author: M. S. Rosenfeld
Publisher: ASTM International
ISBN: 9780803100312
Category : Technology & Engineering
Languages : en
Pages : 264
Book Description
Publisher: ASTM International
ISBN: 9780803100312
Category : Technology & Engineering
Languages : en
Pages : 264
Book Description