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Surface temperature evolution

Fig. 1 Global mean surface temperature evolution during the last century (observed) and projected for the next century. Bars on the right show the possible range of temperature increases from different AOGCM, and also from Simple Climate Models (SCM) and Earth Models of Intermediate Complexity (EMIC). Figure taken from IPCC [1]... Fig. 1 Global mean surface temperature evolution during the last century (observed) and projected for the next century. Bars on the right show the possible range of temperature increases from different AOGCM, and also from Simple Climate Models (SCM) and Earth Models of Intermediate Complexity (EMIC). Figure taken from IPCC [1]...
FIGURE 11.4 Voltage and surface temperature evolution during the test at 25 °C (For colorversion, refer to the plate section.)... [Pg.254]

According to Figure 11.5 and Eqn (A.11.7), the time constant of the surface temperature evolution is equal to ... [Pg.269]

FIGURE 11.4 Voltage and surface temperature evolution during the test at 25 °C. [Pg.625]

In the finite-difference appntach, the partial differential equation for the conduction of heat in solids is replaced by a set of algebraic equations of temperature differences between discrete points in the slab. Actually, the wall is divided into a number of individual layers, and for each, the energy conserva-tk>n equation is applied. This leads to a set of linear equations, which are explicitly or implicitly solved. This approach allows the calculation of the time evolution of temperatures in the wall, surface temperatures, and heat fluxes. The temporal and spatial resolution can be selected individually, although the computation time increa.ses linearly for high resolutions. The method easily can be expanded to the two- and three-dimensional cases by dividing the wall into individual elements rather than layers. [Pg.1067]

Self-Test 1.3B A red giant is a late stage in the evolution of a star. The average wavelength maximum at 700. nm shows that a red giant cools as it dies. What is the surface temperature of a red giant ... [Pg.134]

Since driving force of variations of the volatilisation rate is influenced by the predominant mean sea surface temperature changes of it will influence the evolution of the volatilisation rate and, hence, the distribution of the substance. The influence of the wind speed is expected to increase in a warming climate with higher sea surface temperatures, as it was shown that for high sea surface temperatures the variance is dominated by wind speed changes. [Pg.47]

Courtina R. and Kimb S. J. (2002). Mapping of Titan s tropopause and surface temperatures from Voyager IRIS spectra, Planetary and Space Science 50 309-321. Davis W. L. and McKay C. P. (1996). Origins of Life a comparison of theories and applications to Mars. Origins of Life and Evolution of the Biosphere 26 61-73. [Pg.330]

Figure 1-8 Heat and mass diffusion in a semi-infinite medium in which the diffusion profile propagates according to square root of time, (a) The evolution of temperature profile of oceanic plate. The initial temperature is 1600 K. The surface temperature (at depth = 0) is 275 K. Heat diffusivity is 1 mm /s. (b) The evolution of profile in a mineral. Initial in the mineral is l%o. The surface is 10%o. D= 10 m /s. Figure 1-8 Heat and mass diffusion in a semi-infinite medium in which the diffusion profile propagates according to square root of time, (a) The evolution of temperature profile of oceanic plate. The initial temperature is 1600 K. The surface temperature (at depth = 0) is 275 K. Heat diffusivity is 1 mm /s. (b) The evolution of profile in a mineral. Initial in the mineral is l%o. The surface is 10%o. D= 10 m /s.
Figure 7. A and B. Map and topographic cross-sectional view of sample locations from Shuster et al. s (2005) study of incision of the Kliniklini valley, Coast Mountains, British Columbia. C. Model thermal histories for each sample, derived from 4He/3He evolution of step-heating experiments on proton-irradiated samples, and bulk grain (U-Th)/He dates. Samples from the valley bottom require rapid cooling, from 80 °C to surface temperatures, at 1.8 0.2 Ma, and samples from higher elevations require thermal histories with progressively smaller extents of cooling (beginning at 1.8 Ma) with elevation. The highest sample (TEKI-23) was at surface temperature before the 1.8 Ma cooling event experienced by the other samples. Collectively, these data are interpreted to be the result of -2 km incision at 1.8 Ma. After Shuster et al. (2005). Figure 7. A and B. Map and topographic cross-sectional view of sample locations from Shuster et al. s (2005) study of incision of the Kliniklini valley, Coast Mountains, British Columbia. C. Model thermal histories for each sample, derived from 4He/3He evolution of step-heating experiments on proton-irradiated samples, and bulk grain (U-Th)/He dates. Samples from the valley bottom require rapid cooling, from 80 °C to surface temperatures, at 1.8 0.2 Ma, and samples from higher elevations require thermal histories with progressively smaller extents of cooling (beginning at 1.8 Ma) with elevation. The highest sample (TEKI-23) was at surface temperature before the 1.8 Ma cooling event experienced by the other samples. Collectively, these data are interpreted to be the result of -2 km incision at 1.8 Ma. After Shuster et al. (2005).
Details of this resolution can be found in any heat-transfer book [12]. Figure 3.4 presents a typical set of data that show the evolution of the surface temperature as a function of time. The peaks indicate the moment of ignition. [Pg.55]

Figure 3.13. Temperature evolution of the parameter re T) of the first-surface exciton (hollow circles). The full circles indicate the values obtained for the bulk exciton (Fig. 2.14). The quasi-coincidence at T 0 is fortuitous, but the surface states appear less broadened than the bulk states in the region 30-50 K, which could correspond to a decay at the surface of the density of interplane phonons coupled to the exciton (see Section III.B). Figure 3.13. Temperature evolution of the parameter re T) of the first-surface exciton (hollow circles). The full circles indicate the values obtained for the bulk exciton (Fig. 2.14). The quasi-coincidence at T 0 is fortuitous, but the surface states appear less broadened than the bulk states in the region 30-50 K, which could correspond to a decay at the surface of the density of interplane phonons coupled to the exciton (see Section III.B).
Figure 34 The steps involved in determining the depth of container wall penetration under Canadian nuclear waste disposal conditions using data obtained in an electrochemical galvanic coupling experiment. (A) Crevice propagation rate (R cc Ic) as a function of temperature (T) (B) RCc as a function of 02 concentration [02] (C) calculated evolution of container surface temperatures and vault 02 concentrations with time in the vault (D) flux of 02 (Jo2) to the container surface as a function of time (E) predicted evolution of Rcc up to the time of repassivation (i.e., at [02]p) (F) total extent of crevice corrosion damage expressed as the total amount of 02 consumed (Q) up to the time of repassivation (G) experimentally determined maximum depth of wall penetration (Pw) as a function of 02 consumed (Q) (H) predicted maximum value of Pw up to the time of repassivation (fP)-... Figure 34 The steps involved in determining the depth of container wall penetration under Canadian nuclear waste disposal conditions using data obtained in an electrochemical galvanic coupling experiment. (A) Crevice propagation rate (R cc Ic) as a function of temperature (T) (B) RCc as a function of 02 concentration [02] (C) calculated evolution of container surface temperatures and vault 02 concentrations with time in the vault (D) flux of 02 (Jo2) to the container surface as a function of time (E) predicted evolution of Rcc up to the time of repassivation (i.e., at [02]p) (F) total extent of crevice corrosion damage expressed as the total amount of 02 consumed (Q) up to the time of repassivation (G) experimentally determined maximum depth of wall penetration (Pw) as a function of 02 consumed (Q) (H) predicted maximum value of Pw up to the time of repassivation (fP)-...
Fig. 3.21. Time evolution of the surface temperature of the outer divertor target and the deduced power flux, for typical low density ELMy H-mode conditions in JET (ne,ped = 5.2 1019m 3, Te,pea = 1650eV). For inter-machine comparisons, the duration of the ELM power pulse is characterized by the rise time of the surface temperature during the ELM (tiIrLM), as illustrated in the figure [16,40]... Fig. 3.21. Time evolution of the surface temperature of the outer divertor target and the deduced power flux, for typical low density ELMy H-mode conditions in JET (ne,ped = 5.2 1019m 3, Te,pea = 1650eV). For inter-machine comparisons, the duration of the ELM power pulse is characterized by the rise time of the surface temperature during the ELM (tiIrLM), as illustrated in the figure [16,40]...

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Surface evolution

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