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Accelerated crack growth, residual stress, and a cracked zinc coated pressure shellDuring a partial inspection of a 42 year old, operating, pressurized wind tunnel at NASA-Ames Research Center, a surface connected defect 114 in. long having an indicated depth of a 0.7 in. was detected. The pressure shell, constructed of a medium carbon steel, contains approximately 10 miles of welds and is cooled by flowing water over its zinc coated external surface. Metallurgical and fractographic analysis showed that the actual detect was 1.7 in. deep, and originated from an area of lack of weld penetration. Crack growth studies were performed on the shell material in the laboratory under various loading rates, hold times, and R-ratios with a simulated shell environment. The combination of zinc, water with electrolyte, and steel formed an electrolytic cell which resulted in an increase in cyclic crack growth rate by as much as 500 times over that observed in air. It was concluded that slow crack growth occurred in the pressure shell by a combination of stress corrosion cracking due to the welding residual stress and corrosion fatigue due to the cyclic operating stress.
Document ID
19880044173
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dittman, Daniel L.
(NASA Ames Research Center Moffett Field, CA, United States)
Hampton, Roy W.
(NASA Ames Research Center Moffett Field, CA, United States)
Nelson, Howard G.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Mechanical Engineering
Meeting Information
Meeting: ISTFA 1987 - International Symposium for Testing and Failure Analysis
Location: Los Angeles, CA
Country: United States
Start Date: November 9, 1987
End Date: November 13, 1987
Accession Number
88A31400
Distribution Limits
Public
Copyright
Other

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