Fig. 6.10 Creep strength of several titanium alloys More

Fig. 12.5 Creep strength vs. V f fine γ′ for CGDS MAR-M-200 More

Fig. 4.28 Creep strength (0.5%) vs. temperature of sheet superalloys for combustor applications More

Fig. 4.2 Creep strength of different materials used as boiler tubes and related applications More

Fig. 14.31 Effect of combined Al+Ti content in alloy 800H on the creep strength (1% in 10,000 h and 30,000 h) at 650 and 850 °C (1200 and 1560 °F). Source: Ref 38 More

Fig. 3.2 Creep strength of solid-solution-hardened Inconel 625. Source: Ref 4 More

Fig. 7.111 Dependence of the creep strength of various hot working steels on the testing temperature at various heat treated strengths [ Güm 81 ] More

Fig. 9.40. Gamma-prime overaging and associated loss of creep strength in Udimet 710 tested at 845 °C and 350 MPa (1555 °F and 50 ksi) ( Ref 70 ; courtesy of P. Lowden, Liburdi Engineering, Ltd., Burlington, Canada). Top: New creep life, 140 h. Bottom: Service, 45,000 h; creep life, 10 h. More

Fig. 17.49 Effect of the sum of Al, Si, and Mg contents on the creep strength of hot-pressed beryllium tested at 982 °C (1800 °F) at a strain rate of 10 –4 /s. Source: Borch 1979 More

Fig. 17.50 Effect of BeO dispersion on creep strength of high-purity hot isostatic pressed beryllium. Source: Borch 1979 More

Fig. 20 Relative 100,000-h creep strength More

Fig. 24 General comparison of creep strengths of various creep-resistant low-alloy steels More

Fig. 3.17 Tensile strength and creep resistance of Ti-Al, Ti-AlZr, and Ti-Al-Hf. Ultimate strength rises as the atomic percent of the combined elements increases; creep strength also rises. More

Fig. 3.19 Yield and creep strengths of an alpha alloy Ti-5Al-2.5Sn and an alpha-beta alloy Ti-8Mn are shown for a range of temperatures. More

Fig. 12.65 Typical 1.0% creep strengths for CMSX-10 and CMSX-4 SCDS alloys and CM 186LC and CM 247LC CGDS alloys using Larson-Miller parameter (P LM ). Note: P LM = T (C + log t ) where C = Larson-Miller constant, T = absolute temperature, t = time in h. For this plot, C = 20, T = K More

Fig. 5.51 1% creep strengths of HK-40 and HK-30 tested at 1000 °C (1832 °F) in air, H 2 -1%CH 4 ( a c = 0.8), and for precarburized specimens tested in H 2 -1%CH 4 . Source: Ref 63 More

Fig. 5.10 Comparison of typical 150 h, 0.1% creep strengths reported for various titanium alloys. Source: Ref 5.7 More

Fig. 12.14 Comparison of typical 150 h, 0.1% creep strengths for selected titanium alloys More

Fig. 7.39. Creep-rupture strength of a low-silicon 2¼Cr-1Mo-¼V-Ti-B developmental steel ( Ref 84 ). More

Fig. 9.7. Development of new alloys for increased creep-rupture strength ( Ref 3 ). More