Menu
Search
Filters
Close
Menu

03515 A COMPARISON STUDY OF STRESS CORROSION CRACK GROWTH RATES FOR AA7XXX ALLOYS AS A FUNCTION OF BULK AQUEOUS CHLORIDE CONCENTRATIONS AND SIMULATED CRACK TIP CHEMISTRIES

Picture for 03515 A COMPARISON STUDY OF STRESS CORROSION
Available for download
Product Number: 51300-03515-SG
ISBN: 03515 2003 CP
Author: Brian J. Connolly, Michelle G. Koul, Angela L. Moran
$0.00
$20.00
$20.00
Various alloys are being considered for drop-in replacement and refurbishment of corrosion and stress corrosion cracking prone AA7075-T6 (UNS A97075) components on aging military aircraft. This project evaluates three candidate aluminum alloys that meet mechanical property requirements and are thought to be superior to AA7075-T6 in terms of corrosion performance. The three alloys tested include AA7150-T7751 (UNS A97150), AA7249-T76511, and AA7040-T7651. Environmentally assisted crack growth rates for these alloys were documented and compared to those of AA7075-T6 and AA7075-T73 in various bulk aqueous chloride environments. A study was also performed to elucidate the mechanistic importance of critical crack tip chemistries on the stress corrosion cracking behavior of these 7XXX series alloys. Keywords: aluminum alloys, aging aircraft, stress corrosion cracking, crack tip chemistry
Various alloys are being considered for drop-in replacement and refurbishment of corrosion and stress corrosion cracking prone AA7075-T6 (UNS A97075) components on aging military aircraft. This project evaluates three candidate aluminum alloys that meet mechanical property requirements and are thought to be superior to AA7075-T6 in terms of corrosion performance. The three alloys tested include AA7150-T7751 (UNS A97150), AA7249-T76511, and AA7040-T7651. Environmentally assisted crack growth rates for these alloys were documented and compared to those of AA7075-T6 and AA7075-T73 in various bulk aqueous chloride environments. A study was also performed to elucidate the mechanistic importance of critical crack tip chemistries on the stress corrosion cracking behavior of these 7XXX series alloys. Keywords: aluminum alloys, aging aircraft, stress corrosion cracking, crack tip chemistry
PRICE BREAKS - The more you buy, the more you save
Quantity
1+
5+
Price
$20.00
$20.00
Product tags
Also Purchased
Picture for 03510 STRESS CORROSION CRACKING SUSCEPTIBILITY
Available for download

03510 STRESS CORROSION CRACKING SUSCEPTIBILITY OF ALUMINUM-SILICON-BRONZE

Product Number: 51300-03510-SG
ISBN: 03510 2003 CP
Author: J.J. Hoffman, J.W. Slusser, J.L. O’Leary
$20.00
Picture for 03511 REQUIREMENTS FOR INITIATION OF INTERGRANULAR
Available for download

03511 REQUIREMENTS FOR INITIATION OF INTERGRANULAR SCC IN DHP-COPPER TUBES

Product Number: 51300-03511-SG
ISBN: 03511 2003 CP
Author: Gregor Mori, Doris Scherer, Sandra Schwentenwein
$20.00
Picture for 03513 ROLE OF HYDROGEN IN STRESS CORROSION
Available for download

03513 ROLE OF HYDROGEN IN STRESS CORROSION CRACKING OF LOW-STRENGTH AL-MG ALLOYS

Product Number: 51300-03513-SG
ISBN: 03513 2003 CP
Author: R.H. Jones, M.J. Danielson
$20.00
Categories
Industry
Recently viewed
Popular tags
View all

Association for Materials Protection and Performance

© AMPP All Rights Reserved.
Membership Terms of Content Use
Contact Customer Support