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The Relative Stress-Corrosion Cracking Susceptibility of Candidate Aluminum-Lithium Alloys for Aerospace Applications

Patrick P. Pizzo ; prepared for Ames Research Center under contract NAS2-10365
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1982.
Language
English
Series
NASA Contractor Report
SuDoc Number
NAS 1.26:3578
Description
123 p. : ill. ; 28 cm.
Notes
  • "Advanced Research and Applications Corporation."
  • "June 1982"--Cover.
  • Includes bibliographical references.
Series Statement
NASA contractor report 3578
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| The relative stress-corrosion cracking susceptibility of candidate aluminum-lithium alloys for aerospace applications / c| Patrick P. Pizzo ; prepared for Ames Research Center under contract NAS2-10365.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, Scientific and Technical Information Office ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1982.
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    a| Corrosion and anti-corrosives.
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    a| Stress corrosion.
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