Accession Number:

AD0701789

Title:

ENGINEERING PRACTICE TO AVOID STRESS CORROSION CRACKING

Descriptive Note:

Conference proceedings

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

• Forsyth, P.
• Jaffee, R. I.
• Brown, R. J.
• Steigerwald, E. A.

Report Date:

1970-02-01

Pagination or Media Count:

207.0

Abstract:

Contents The examination of service failures The relative influence of stress and environment on titanium The relative influence of stress and environment on aluminium Characteristics of environmentally-induced delayed failure in high strength steels Etude du comportement de lalliage magnesium -8 Daluminium en corrosion sous tension The relation between test results and service experience Sustained stresses and their effect on stress corrosion cracking Residual stresses arising from machining and fabrication Stress corrosion tests on welded cruciforms of 7039-type aluminum alloy The application of N.D.T. techniques to the problem of stress corrosion cracking The choice of materials The environment encountered in aircraft service The influence of surface and protective treatments on stress corrosion behaviour Methods of communication about preventive action - the strategy of stress corrosion cracking prevention Status of research on stress corrosion cracking Determination of residual stresses by indentation hardness testing A review of non-destructive methods for evaluation of residual stress and stress corrosion German experience in x-ray inspection.

Descriptors:

• *CORROSION INHIBITION
• *AIRFRAMES
• *STRESS CORROSION
• STRESSES
• SYMPOSIA
• NONDESTRUCTIVE TESTING
• ALUMINUM ALLOYS
• CRACKS
• STEEL
• FAILURE(MECHANICS)
• TITANIUM ALLOYS
• PROTECTIVE TREATMENTS

Subject Categories:

• Aircraft
• Properties of Metals and Alloys

Distribution Statement:

APPROVED FOR PUBLIC RELEASE