The Growth of Small Corrosion Fatigue Cracks in Alloy 2024
Author : Robert S. Piascik
Publisher :
Page : 34 pages
File Size : 14,59 MB
Release : 1993
Category : Aluminum alloys
ISBN :
Author : Robert S. Piascik
Publisher :
Page : 34 pages
File Size : 14,59 MB
Release : 1993
Category : Aluminum alloys
ISBN :
Author : Charles E. Harris
Publisher :
Page : 520 pages
File Size : 15,32 MB
Release : 1994
Category : Airframes
ISBN :
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 32 pages
File Size : 11,24 MB
Release : 2018-07-13
Category :
ISBN : 9781722867089
The corrosion fatigue crack growth characteristics of small surface and corner cracks in aluminum alloy 2024 is established. The damaging effect of salt water on the early stages of small crack growth is characterized by crack initiation at constituent particle pits, intergranular microcracking for a less than 100 micrometers, and transgranular small crack growth for a micrometer. In aqueous 1 percent NaCl and at a constant anodic potential of -700 mV(sub SCE), small cracks exhibit a factor of three increase in fatigue crack growth rates compared to laboratory air. Small cracks exhibit accelerated corrosion fatigue crack growth rates at low levels of delta-K (less than 1 MPa square root of m) below long crack delta-K (sub th). When exposed to Paris regime levels of crack tip stress intensity, small corrosion fatigue cracks exhibit growth rates similar to that observed for long cracks. Results suggest that crack closure effects influence the corrosion fatigue crack growth rates of small cracks (a less than or equal to 100 micrometers). This is evidenced by similar small and long crack growth behavior at various levels of R. Contrary to the corrosion fatigue characteristics of small cracks in high strength steels, no pronounced chemical crack length effect is observed for Al by 2024 exposed to salt water. Piascik, Robert S. and Willard, Scott A. Langley Research Center RTOP 538-02-10-01...
Author : C. E. Harris
Publisher :
Page : 28 pages
File Size : 36,31 MB
Release : 2000
Category : Airframes
ISBN :
An extensive experimental database has been assembled from very detailed teardown examinations of fatigue cracks found in rivet holes of fuselage structural components. Based on this experimental database, a comprehensive analysis methodology was developed to predict the onset of widespread fatigue damage in lap joints of fuselage structure. Several computer codes were developed with specialized capabilities to conduct the various analyses that make up the comprehensive methodology. Over the past several years, the authors have interrogated various aspects of the analysis methods to determine the degree of computational rigor required to produce numerical predictions with acceptable engineering accuracy. This study led to the formulation of a practical engineering approach to predicting fatigue crack growth in riveted lap joints. This paper describes the practical engineering approach and compares predictions with the results from several experimental studies.
Author : William Alan Van der Sluys
Publisher : ASTM International
Page : 304 pages
File Size : 32,44 MB
Release : 1997
Category : Metals
ISBN : 0803124082
Author :
Publisher :
Page : 568 pages
File Size : 25,61 MB
Release : 1972
Category : Mechanics, Applied
ISBN :
Author :
Publisher :
Page : 702 pages
File Size : 24,70 MB
Release : 1995
Category : Aeronautics
ISBN :
Author : Claude Bathias
Publisher : John Wiley & Sons
Page : 415 pages
File Size : 43,52 MB
Release : 2013-03-04
Category : Technology & Engineering
ISBN : 1118623371
The design of mechanical structures with improved and predictable durability cannot be achieved without a thorough understanding of the mechanisms of fatigue damage and more specifically the relationships between the microstructure of materials and their fatigue properties. Written by leading experts in the field, this book (which is complementary to Fatigue of Materials and Structures: Application to Damage and Design, also edited by Claude Bathias and André Pineau), provides an authoritative, comprehensive and unified treatment of the mechanics and micromechanisms of fatigue in metals, polymers and composites. Each chapter is devoted to one of the major classes of materials or to different types of fatigue damage, thereby providing overall coverage of the field. The book deals with crack initiation, crack growth, low-cycle fatigue, gigacycle fatigue, shorts cracks, fatigue micromechanisms and the local approach to fatigue damage, corrosion fatigue, environmental effects and variable amplitude loadings, and will be an important and much used reference for students, practicing engineers and researchers studying fracture and fatigue in numerous areas of mechanical, structural, civil, design, nuclear, and aerospace engineering as well as materials science.
Author : G.C. Sih
Publisher : Springer Science & Business Media
Page : 467 pages
File Size : 32,21 MB
Release : 2007-11-29
Category : Science
ISBN : 1402050623
For the first time, a book is being edited to address how results from one scale can be shifted or related to another scale, say from macro to micro or vice versa. The new approach retains the use of the equilibrium mechanics within a scale level such that cross scale results can be connected by scale invariant criteria. Engineers in different disciplines should be able to understand and use the results.
Author : Norbert G. H. Meyendorf
Publisher : Springer Science & Business Media
Page : 435 pages
File Size : 11,68 MB
Release : 2013-11-21
Category : Science
ISBN : 3662089882
With an emphasis on aircraft materials, this book describes techniques for the material characterization to detect and quantify degradation processes such as corrosion and fatigue. It introduces readers to these techniques based on x-ray, ultrasonic, optical and thermal principles and demonstrates the potential of the techniques for a wide variety of applications concerning aircraft materials, especially aluminum and titanium alloys. The advantages and disadvantages of various techniques are evaluated.