Author: Ralph Ivan StephensPublisher:
ISBN: 9780898836875
Category : Technology & Engineering
Languages : en
Pages : 102
Book Description
Fatigue and Fracture Toughness of A356-T6 Cast Aluminum Alloy
Author: Ralph Ivan StephensPublisher:
ISBN: 9780898836875
Category : Technology & Engineering
Languages : en
Pages : 102
Book Description
Fatigue and Fracture Toughness of Water-chilled A356-T6 Cast Aluminum Alloy
Author: Brian J. MahoneyPublisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 168
Book Description
Data Sheet on Fracture Toughness and High-cycle Fatigue Properties of Aluminum Alloy A356-T6 Cast Material
Author: 物質材料研究機構Data sheet on fracture toughness and high-cycle fatigue properties of aluminium alloy A356-T6 cast materials
Author: Data sheet on fatigue crack growth properties of cast A356-T6 aluminum alloy
Author: Fracture Resistance of Aluminum Alloys
Author: John Gilbert KaufmanPublisher: ASM International
ISBN: 1615030611
Category : Technology & Engineering
Languages : en
Pages : 235
Book Description
Annotation Kaufman prevents this summary of data on the fracture characteristics of aluminum alloys, broadly based on a publication by Alcoa in 1964, Fracture Characteristics of Aluminum Alloys. Coverage includes tensile properties as indicators of fracture behavior; notched-bar impact and related tests for toughness; notch toughness and sensitivity; tear resistance; fracture toughness; the interrelation of fracture characteristics; toughness at subzero and elevated temperatures; subcritical crack growth; and metallurgical considerations in fracture resistance. Most of the data is presented in only the English/engineering units, contrary to normal ASM International and Aluminum Association, Inc. policies. The author's credentials are not stated. c. Book News Inc
Effect of Service Usage on Tensile, Fatigue, and Fracture Properties of 7075-T6 and 7178-T6 Aluminum Alloys
Author: Richard A. EverettPublisher:
ISBN:
Category : Airframes
Languages : en
Pages : 36
Book Description
Fatigue Crack Propagation in 2024-T3 and 7075-T6 Aluminum Alloys at High Stresses
Author: Robert G. DubenskyPublisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 36
Book Description
Effect of Stress Ratio on Fatigue-crack Growth in 7075-T6 and 2024-T3 Aluminum-alloy Specimens
Author: C. M. HudsonPublisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 36
Book Description
Stress ratio effects on fatigue crack growth in sheet aluminum alloys.
Effects of Changing Stress Amplitude on the Rate of Fatigue-crack Propagation in Two Aluminum Alloys
Author: C. M. HudsonPublisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 28
Book Description
A series of fatigue tests with specimens subjected to constant amplitude and two-step axial loads were conducted on 12-inch-wide sheet specimens of 2024-T3 and 7075-T6 aluminum alloy to study the effects of a change in stress level on fatigue-crack propagation. Comparison of the results of the tests in which the specimens were tested at first a high and then a low stress level with those of the constant-stress-amplitude tests indicated that crack propagation was generally delayed after the transition to the lower stress level. In the tests in which the specimens were tested at first a low and then a high stress level, crack propagation continued at the expected rate after the change in stress levels.