Fatigue Crack Growth Rate Test Results for Al-Li 2195 Parent Metal, Variable Polarity Plasma Arc Welds and Friction Stir Welds

Fatigue Crack Growth Rate Test Results for Al-Li 2195 Parent Metal, Variable Polarity Plasma Arc Welds and Friction Stir Welds
Title Fatigue Crack Growth Rate Test Results for Al-Li 2195 Parent Metal, Variable Polarity Plasma Arc Welds and Friction Stir Welds PDF eBook
Author Robert A. Hafley
Publisher
Total Pages 46
Release 2000
Genre Aluminum alloys
ISBN

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The fatigue crack growth rate of aluminum-lithium (Al-Li) alloy 2195 plate and weldments was determined at 200°F, ambient temperature and -320°F. The effects of stress ratio (R), welding process, orientation and thickness were studied. Results are compared with plate data from the Space Shuttle Super Lightweight Tank (SLWT) allowables program. Data from the current series of tests, both plate and weldment, falls within the range of data generated during the SLWT allowables program.

Fatigue Crack Growth Rate Test Results for Al-Li 2195 Parent Metal, Variable Polarity Plasma Arc Welds and Friction Stir Welds

Fatigue Crack Growth Rate Test Results for Al-Li 2195 Parent Metal, Variable Polarity Plasma Arc Welds and Friction Stir Welds
Title Fatigue Crack Growth Rate Test Results for Al-Li 2195 Parent Metal, Variable Polarity Plasma Arc Welds and Friction Stir Welds PDF eBook
Author National Aeronautics and Space Administration (NASA)
Publisher Createspace Independent Publishing Platform
Total Pages 44
Release 2018-05-31
Genre
ISBN 9781720523376

Download Fatigue Crack Growth Rate Test Results for Al-Li 2195 Parent Metal, Variable Polarity Plasma Arc Welds and Friction Stir Welds Book in PDF, Epub and Kindle

The fatigue crack growth rate of aluminum-lithium (Al-Li) alloy 2195 plate and weldments was determined at 200-F, ambient temperature and -320-F. The effects of stress ratio (R), welding process, orientation and thickness were studied. Results are compared with plate data from the Space Shuttle Super Lightweight Tank (SLWT) allowables program. Data from the current series of tests, both plate and weldment, falls within the range of data generated during the SLWT allowables program.Hafley, Robert A. and Wagner, John A. and Domack, Marcia S.Langley Research CenterALUMINUM-LITHIUM ALLOYS; CRACK PROPAGATION; WELDED JOINTS; WELD TESTS; CRACKING (FRACTURING); FATIGUE (MATERIALS); CRACKS; PLASMA ARC WELDING; FRICTION WELDING; REUSABLE LAUNCH VEHICLES

NASA Langley Scientific and Technical Information Output 2000

NASA Langley Scientific and Technical Information Output 2000
Title NASA Langley Scientific and Technical Information Output 2000 PDF eBook
Author
Publisher
Total Pages 162
Release 2001
Genre
ISBN

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A Study of Friction Stir Welded 2195 Al-Li Alloy by the Scanning Reference Electrode Technique

A Study of Friction Stir Welded 2195 Al-Li Alloy by the Scanning Reference Electrode Technique
Title A Study of Friction Stir Welded 2195 Al-Li Alloy by the Scanning Reference Electrode Technique PDF eBook
Author Merlin D. Danford
Publisher
Total Pages 20
Release 1998
Genre Aluminum alloys
ISBN

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A study of the corrosion of friction stir welded 2195 Al-Li alloy has been carried out using the scanning reference electrode technique (SRET). The results are compared to those obtained from a study of heterogeneously welded samples.

Flaw Growth Behavior in Thick Welded Plates of 2219-T87 Aluminum at Room and Cryogenic Temperatures

Flaw Growth Behavior in Thick Welded Plates of 2219-T87 Aluminum at Room and Cryogenic Temperatures
Title Flaw Growth Behavior in Thick Welded Plates of 2219-T87 Aluminum at Room and Cryogenic Temperatures PDF eBook
Author Royce G. Forman
Publisher
Total Pages 54
Release 1973
Genre Aluminum alloys
ISBN

Download Flaw Growth Behavior in Thick Welded Plates of 2219-T87 Aluminum at Room and Cryogenic Temperatures Book in PDF, Epub and Kindle

Axial load fatigue and fracture tests were conducted on thick welded plates of 2219-T87 aluminum alloy to determine the tensile strength properties and the flaw growth behavior in electron beam, gas metal arc, and pulse current gas tungsten arc welds for plates 6.35 centimeters (2.5 in.) thick. The tests were conducted in room temperature air and in liquid nitrogen environments. Specimens were tested in both the as-welded and the aged after welding conditions. The experimental crack growth rate were correlated with theoretical crack growth rate predictions for semielliptical surface flaws.

Fatigue and Fracture Testing of Weldments

Fatigue and Fracture Testing of Weldments
Title Fatigue and Fracture Testing of Weldments PDF eBook
Author Harry I. McHenry
Publisher ASTM International
Total Pages 310
Release 1990
Genre Welded joints
ISBN 0803112777

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Fifteen papers from a symposium held in Sparks, Nev., April 1988. They cover: low and high cycle fatigue, fatigue crack growth, corrosion fatigue, fracture toughness testing, and wide-plate testing. Annotation copyright Book News, Inc. Portland, Or.

Fatigue Testing of Weldments

Fatigue Testing of Weldments
Title Fatigue Testing of Weldments PDF eBook
Author D. W. Hoeppner
Publisher ASTM International
Total Pages 304
Release 1978
Genre Technology & Engineering
ISBN 9780803103481

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