1-20 of 652

Search Results for aging response curves

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Image
Published: 01 January 1990
Fig. 17 Aging response curves for beryllium-nickel alloy N03360 strip More
Image
Published: 01 June 2016
Fig. 26 Aging response curves for low-beryllium, moderate-strength, and high-thermal-conductivity cast and solution-treated alloy C82000 (97wt%Cu-2.5wt%Co-0.5wt%Be). Source: Ref 11 More
Image
Published: 01 June 2016
Fig. 14 Aging-response curves for beryllium-nickel alloy N03360 strip. Source: Ref 15 More
Image
Published: 01 January 1990
Fig. 4 Age-hardening response curves for the tensile strength, yield strength, and elongation of C17200. (a) Annealed (TB00) temper. (b) Roll-hardened (TD04) temper More
Image
Published: 01 January 1990
Fig. 5 Age-hardening response curves for annealed (TB00 temper) C17510 More
Image
Published: 01 June 2016
Fig. 23 Age-hardening response curves for tensile strength, yield strength, and elongation of alloy C17200 (Cu-1.8 to 2.2 wt% Be-0.20 wt% min Co plus nickel). (a) Annealed (TB00 temper) and (b) roll-hardened (TD04 temper) conditions. Source: Ref 8 More
Image
Published: 01 June 2016
Fig. 24 Age-hardening response curves for tensile strength, yield strength, and elongation of alloy C17510 (Cu-0.2 to 0.6 wt% Be-1.4 to 2.2 wt% Ni). Source: Ref 8 More
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006560
EISBN: 978-1-62708-210-5
... 151 3. Aging Response Curves of Aluminum Casting Alloys , Approved by the ASM Handbook Committee for addition to the ASM Handbook, 2011 4. Kaufman J.G. and Rooy E.L. , Aluminum Alloy Castings: Properties, Processes, and Applications , ASM International , 2004 , p 133 – 173 ...
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001071
EISBN: 978-1-62708-162-7
... aging response curves for solution-annealed and annealed and cold worked C17200 are shown in Fig. 4 . When age hardened at 315 to 335 °C (600 to 635 °F), strength increases to a plateau in about 3 h for annealed material or about 2 h for cold-worked material and remains essentially constant thereafter...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006281
EISBN: 978-1-62708-169-6
.... Bronzes originally (from the time of the Bronze Age) referred to alloys in which tin was the major alloying element. Today (2016), however, the term bronze is commonly used for a number of alloys that contain other elements with little, if any, tin. Bronzes can refer to copper alloys with various...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006271
EISBN: 978-1-62708-169-6
... and simulation of age hardening as being the most important heat treatment to strengthen aluminum alloys. It provides information on the heat treatment simulation model, the yield strength model based on the responsible strengthening mechanisms, and the flow curve model based on mechanical tests. The article...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002411
EISBN: 978-1-62708-193-1
..., and spinodal alloys. It discusses the fatigue testing of the copper alloys and tabulates the tensile and fatigue strengths of the copper alloys. The article schematically illustrates S-N curves for the solid-solution (non-aging) strengthened alloys. It concludes with a discussion on the role of microstructure...
Image
Published: 01 December 2004
Fig. 42 Time-temperature diagram of precipitation responses of an aluminum-lithium alloy (alloy 8090) for volume formation of the S phase (Al 2 CuMg). This practical isothermal transformation curve is based on a real commercial-sized component that has been exposed to aging temperatures More
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002396
EISBN: 978-1-62708-193-1
... + ( σ a K ′ ) 1 / n ′ where E is the elastic modulus and K ′ and n ′ are cyclic deformation properties. This formulation allows for direct comparison with monotonic tension curves so that cyclic-hardening or cyclic-softening responses can be quickly assessed. Monotonic...
Series: ASM Handbook
Volume: 11B
Publisher: ASM International
Published: 15 May 2022
DOI: 10.31399/asm.hb.v11B.a0006921
EISBN: 978-1-62708-395-9
... several important steps: Define what constitutes a failure Identify the aging mechanism that is likely to be the long-term material behavior response leading to the failure Collect short-term data under test conditions that most closely resemble the use conditions Utilize temperature...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002404
EISBN: 978-1-62708-193-1
...) are identical to the semidynamic curves, indicating that the beneficial effects are maintained at very high strain rates ( Ref 94 ). One of the two type 304 heats studied by Marschall ( Ref 96 ) shows a similar response, with J c increasing by 15% under semidynamic conditions. The second heat shows a much...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006261
EISBN: 978-1-62708-169-6
.... The precipitation of γ′ causes strengthening, as shown in Fig. 4 . The aging curve has the shape typical of that associated with precipitation hardening, passing through a maximum with time at the aging temperature. Strengthening occurs from the elastic interface strains with the lattice parameter mismatch...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006263
EISBN: 978-1-62708-169-6
... response of titanium alloys. This factor is even more critical in weakly β-stabilized systems where transformation of the β phase occurs more readily during a quench. The effect of quench delay is shown in Fig. 22 for Ti-6Al-4V bar that was subsequently aged at 480 °C (900 °F...
Series: ASM Handbook
Volume: 24A
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.hb.v24A.a0006952
EISBN: 978-1-62708-439-0
... the correlation between microstructure/texture and dynamic impact response of the as-built and heat treated materials. True stress/true strain curves of dynamically deformed as-built L-PBF maraging steel samples at strain rates of 1500, 2000, 3200, 3500, and 4000 s −1 are presented in Fig. 7(a) . Both...
Series: ASM Handbook
Volume: 14B
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v14b.a0005133
EISBN: 978-1-62708-186-3
... temperatures (120 to 190 °C, or 250 to 375 °F). Because creep is the phenomenon responsible for achieving the part shape, age forming is sometimes referred to as creep forming. The most common application for age forming is the shaping of upper wing skins in the aerospace industry. Recent investigations ( Ref...