Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminium Sheet at -320 Degrees F (77 K)

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminium Sheet at -320 Degrees F (77 K) PDF Author: William S. Pierce
Publisher:
ISBN:
Category :
Languages : en
Pages : 41

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Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminium Sheet at -320 Degrees F (77 K)

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminium Sheet at -320 Degrees F (77 K) PDF Author: William S. Pierce
Publisher:
ISBN:
Category :
Languages : en
Pages : 41

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Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -320° F (77 K)

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -320° F (77 K) PDF Author: William S. Pierce
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 0

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Book Description
An investigation was conducted to determine the low-cycle (under 10 000 cycles) crack growth characteristics of through- center- cracked specimens 0.060 in. (0.152 cm) thick subjected to tension-tension cyclic loading. The following factors were studied: (1) minimum to maximum initial stress intensity ratio R (sub i); (2) the maximum gross stress applied, as percentage of critical fracture stress; and (3) cyclic rate. The crack growth rate was found to be a function of stress level expressed as percentage of critical fracture stress for specimens tested at the same R. value. A crack growth relation was developed which takes into account changes in R. in the low-cycle region. When the cycle rate was decreased from 0. 5 to 0.05 Ha, the cyclic life was reduced, but only for high initial stress intensities.

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -3200 F (77 K)

Factors Influencing Low-cycle Crack Growth in 2014-T6 Aluminum Sheet at -3200 F (77 K) PDF Author: William S. Pierce
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 52

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Factors Influencing Low-Cycle Crack Growth in 2014-T6 Aluminum Sheet at -320 F (77 K).

Factors Influencing Low-Cycle Crack Growth in 2014-T6 Aluminum Sheet at -320 F (77 K). PDF Author: William S. Pierce
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 45

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Book Description
An investigation was conducted to determine the low-cycle (under 10 000 cycles) crack growth characteristics of through- center- cracked specimens 0.060 in. (0.152 cm) thick subjected to tension-tension cyclic loading. The following factors were studied: (1) minimum to maximum initial stress intensity ratio R (sub i); (2) the maximum gross stress applied, as percentage of critical fracture stress; and (3) cyclic rate. The crack growth rate was found to be a function of stress level expressed as percentage of critical fracture stress for specimens tested at the same R. value. A crack growth relation was developed which takes into account changes in R. in the low-cycle region. When the cycle rate was decreased from 0. 5 to 0.05 Ha, the cyclic life was reduced, but only for high initial stress intensities.

Crack Growth in 2014-T6 Aluminum Tensile and Tank Specimens Cyclically Loaded at Cryogenic Temperatures

Crack Growth in 2014-T6 Aluminum Tensile and Tank Specimens Cyclically Loaded at Cryogenic Temperatures PDF Author: William S. Pierce
Publisher:
ISBN:
Category : Aluminum
Languages : en
Pages : 44

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Microstructure And Properties Of Materials, Vol 2

Microstructure And Properties Of Materials, Vol 2 PDF Author: James C M Li
Publisher: World Scientific Publishing Company
ISBN: 9813105658
Category : Technology & Engineering
Languages : en
Pages : 454

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Book Description
This is the second volume of an advanced textbook on microstructure and properties of materials. (The first volume is on aluminum alloys, nickel-based superalloys, metal matrix composites, polymer matrix composites, ceramics matrix composites, inorganic glasses, superconducting materials and magnetic materials). It covers titanium alloys, titanium aluminides, iron aluminides, iron and steels, iron-based bulk amorphous alloys and nanocrystalline materials.There are many elementary materials science textbooks, but one can find very few advanced texts suitable for graduate school courses. The contributors to this volume are experts in the subject, and hence, together with the first volume, it is a good text for graduate microstructure courses. It is a rich source of design ideas and applications, and will provide a good understanding of how microstructure affects the properties of materials.Chapter 1, on titanium alloys, covers production, thermomechanical processing, microstructure, mechanical properties and applications. Chapter 2, on titanium aluminides, discusses phase stability, bulk and defect properties, deformation mechanisms of single phase materials and polysynthetically twinned crystals, and interfacial structures and energies between phases of different compositions. Chapter 3, on iron aluminides, reviews the physical and mechanical metallurgy of Fe3Al and FeAl, the two important structural intermetallics. Chapter 4, on iron and steels, presents methodology, microstructure at various levels, strength, ductility and strengthening, toughness and toughening, environmental cracking and design against fracture for many different kinds of steels. Chapter 5, on bulk amorphous alloys, covers the critical cooling rate and the effect of composition on glass formation and the accompanying mechanical and magnetic properties of the glasses. Chapter 6, on nanocrystalline materials, describes the preparation from vapor, liquid and solid states, microstructure including grain boundaries and their junctions, stability with respect to grain growth, particulate consolidation while maintaining the nanoscale microstructure, physical, chemical, mechanical, electric, magnetic and optical properties and applications in cutting tools, superplasticity, coatings, transformers, magnetic recordings, catalysis and hydrogen storage.

Fatigue of Aircraft Structures

Fatigue of Aircraft Structures PDF Author: United States. Naval Air Systems Command
Publisher:
ISBN:
Category :
Languages : en
Pages : 360

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Atlas of Fatigue Curves

Atlas of Fatigue Curves PDF Author: Howard E. Boyer
Publisher: ASM International
ISBN: 9780871702142
Category : Technology & Engineering
Languages : en
Pages : 544

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Book Description
Contains more than 500 fatigue curves for industrial ferrous and nonferrous alloys. Also includes an explanation of fatigue testing and interpretation of test results. Each curve is presented independently and includes an explanation of its particular importance.

Fatigue Crack Growth

Fatigue Crack Growth PDF Author: Hans Albert Richard
Publisher: Springer
ISBN: 3319325345
Category : Technology & Engineering
Languages : en
Pages : 305

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Book Description
This book offers a concise introduction to fatigue crack growth, based on practical examples. It discusses the essential concepts of fracture mechanics, fatigue crack growth under constant and variable amplitude loading and the determination of the fracture-mechanical material parameters. The book also introduces the analytical and numerical simulation of fatigue crack growth as well as crack initiation. It concludes with a detailed description of several practical case studies and some exercises. The target group includes graduate students, researchers at universities and practicing engineers.

Light Metal Alloys Applications

Light Metal Alloys Applications PDF Author: Waldemar Alfredo Monteiro
Publisher: BoD – Books on Demand
ISBN: 953511588X
Category : Technology & Engineering
Languages : en
Pages : 254

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Book Description
Lightweight alloys have become of great importance in engineering for construction of transportation equipment. At present, the metals that serve as the base of the principal light alloys are aluminum and magnesium. One of the most important lightweight alloys are the aluminum alloys in use for several applications (structural components wrought aluminum alloys, parts and plates). However, some casting parts that have low cost of production play important role in aircraft parts. Magnesium and its alloys are among the lightest of all metals and the sixth most abundant metal on earth. Magnesium is ductile and the most machinable of all metals. Many of these light weight alloys have appropriately high strength to warrant their use for structural purposes, and as a result of their use, the total weight of transportation equipment has been considerably decreased.