Record Details
| Fatigue-crack-propagation and fracture- toughness characteristics of 7079 aluminum- alloy sheets and plates in three aged conditions | |||||||
| NTRS Full-Text: | Click to View [PDF Size: 12.1 MB] | ||||||
| Author and Affiliation: |
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| Abstract: | Fatigue crack propagation and fracture toughness characteristics of 7079 aluminum alloys in underage, peak age, and overaged conditions | ||||||
| Publication Date: | Feb 01, 1968 | ||||||
| Document ID: |
19680006007
(Acquired Nov 22, 1995)
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| Accession Number: | 68N15476 | ||||||
| Subject Category: | STRUCTURAL MECHANICS | ||||||
| Report/Patent Number: | NASA-CR-996 | ||||||
| Document Type: | Technical Report | ||||||
| Publisher Information: | NASA, WASHINGTON, United States | ||||||
| Contract/Grant/Task Num: | NAS1-6474 | ||||||
| Financial Sponsor: | NASA; United States | ||||||
| Organization Source: | Boeing Co.; Renton, WA, United States | ||||||
| Description: | 96p; In English | ||||||
| Distribution Limits: | Unclassified; Publicly available; Unlimited | ||||||
| Rights: | No Copyright | ||||||
| NASA Terms: | ALUMINUM ALLOYS; CRACK PROPAGATION; FATIGUE (MATERIALS); FRACTURE STRENGTH; AGING (METALLURGY); CHARPY IMPACT TEST; HEAT TREATMENT; TEMPERATURE EFFECTS | ||||||