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Surfaces emission distribution

Investigations on the emission properties of INSs started quite a long time ago, mainly in connection with the X-ray emission from PSRs. In the seventies it was a common wisdom that the radiation emitted by INSs comes directly from their solid crust and is very close to a blackbody. Lenzen and Trumper (1978) and Brinkmann (1980) were the first to address in detail the issue of the spectral distribution of INS surface emission. Their main result was that... [Pg.61]

Muller, J.-F. Geographical Distribution and Seasonal Variation of Surface Emissions and Deposition Velocities of Atmospheric Trace Gases, J. Geophys. Res., 97, 3787-3804 (1992). [Pg.41]

Upon particle impact, energy is deposited into a surface and distributed through momentum transfer and vibrational and rotational excitation. This leads to heating, electron and photon emission, neutral particle emission, and ion emission. [Pg.20]

Emissions are independent of the tracer concentration and can be considered as a surface flux. The injection of the emissions is integral part of the diffusion scheme in MOZART-3, i.e. as lower boundary for the fluxes, whereas TM5 and MOCAGE distribute the injected mass in a fixed ratio over selected layers in the boundary layer and apply their diffusion operator after the injection. The tendencies of the emissions P, therefore, have to be formulated either as 3D field including the diffusion or as 2D flux term. The diffusion in the IFS would have to be switched off if the 3D emissions-diffusion tendencies are applied. Air bom emissions such as the ones from aircraft would have to be included in the 3D chemistry tendencies, if the surface emissions are expressed as a flux. [Pg.117]

Near rich limits of hydrocarbon flames, soot is sometimes produced in the flame. The carbonaceous particles—or any other solid particles— easily can be the most powerful radiators of energy from the flame. The function k(t) is difficult to compute for soot radiation for use in equation (21) because it depends on the histories of number densities and of size distributions of the particles produced for example, an approximate formula for Ip for spherical particles of radius with number density surface emissivity 6, and surface temperature is Ip = Tl nrle ns) [50]. These parameters depend on the chemical kinetics of soot production—a complicated subject. Currently it is uncertain whether any of the tabulated flammability limits are due mainly to radiant loss (since convective and diffusive phenomena will be seen below to represent more attractive alternatives), but if any of them are, then the rich limits of sooting hydrocarbon flames almost certainly can be attributed to radiant loss from soot. [Pg.281]

The total electron emission yield is the sum of two contributions, one due to the secondary electrons excited by the primary electrons (SEl highly localised at the probe impact zone), the other due to the secondary electrons excited by the backscattered electrons on their return path to the surface (SE2 distributed more diffusely around a point of impact in the case of a light target, cf. Fig. 7.5). The number of secondary electrons created by a backscattered electron is typically two to four times higher than the number created by an incident electron. [Pg.133]

Fig. 16 SEM micrographs of the surface of rupture of ternary blends with type A fibres (a) or type B fibres (b) and the associated acoustic emission distribution curves (a ) or (b ). Fig. 16 SEM micrographs of the surface of rupture of ternary blends with type A fibres (a) or type B fibres (b) and the associated acoustic emission distribution curves (a ) or (b ).
FIGURE 7.8 Example 7,2 spectral emissivity distribution of the spectrally selective surface. [Pg.575]

Because of the stability of HF, the atmospheric densities of F and FO are very small and the effect of fluorine on odd oxygen is insignificant. The reaction of HF with 0(1D) is chemically possible, but is negligible due to the low abundance of this excited atom. The distribution of HF is therefore largely determined by the rates of the surface emission of fluorine containing gases, of photochemical destruction of these gases, and atmospheric dynamics. [Pg.374]

The Arctic contamination potential (AGP) focuses specifically on chemicals that tend to accumulate in Arctic surface media and has therefore been defined as the ratio of the substance mass in Arctic surface media (all media except the atmosphere) divided by the total emissions of substance after 1 (eACP-1) or 10 (eACP-10) years. The emission distribution on the globe is mostly assumed to be proportional to population density. Previously, the Arctic contamination potential has also been defined as the ratio in Arctic surface media divided by the overall mass on the earth (mACP) [36]. In the context of transformation products, the eACP is preferred over the mACP. [Pg.132]

The variable power x on the exponential prefactor (which determines the spectral rise at low energy) arises from (a) statistical shape variations which affect the actual barriers, (b) a mixture of volume and surface emission, (c) the emission of more complex nuclei that subsequently decay into the channel of interest, and (d) quantum penetration. The first factor is the most important, and thus in fitting spectra, often a distribution of Be values is required. [Pg.192]

As a summary of charge distribution after nuclear decay, Fig. 24.3 shows various cases in monatomic or polyatomic gases (inclusive of solid surface emission for a decay and heavy ion nuclear reaction). [Pg.1342]

The mechanism of vessel failure appears to be a two-step process The formation of an initiating overpressure crack in the high-temperature, vapor-wetted walls of the vessel, followed by the final catastrophic unzipping of the containment and a nearly instantaneous release of its contents. The distribution and hashing of the lading causes a fireball if the contents are flammable. The failure of the vessel and the surface emissive power of the BLEVE fireball do not appear to be directly related to the superheat of the contents at failure and indeed may be most severe for conditions when the vessel fails while undergoing a pressure reduction at low superheat. [Pg.470]

Mtiller JF (1992) Geographical-distribution and seasonal-variation of surface emissions and deposition velocities of atmospheric trace gases. J Geophys Res Atmos 97 3787-3804... [Pg.91]

IRE Infrared emission [110] Infrared emission from a metal surface is affected in angular distribution by adsorbed species Orientation of adsorbed molecules... [Pg.314]

Figure Al.7.12. Secondary electron kinetic energy distribution, obtained by measuring the scadered electrons produced by bombardment of Al(lOO) with a 170 eV electron beam. The spectrum shows the elastic peak, loss features due to the excitation of plasmons, a signal due to the emission of Al LMM Auger electrons and the inelastic tail. The exact position of the cutoff at 0 eV depends on die surface work fimction. Figure Al.7.12. Secondary electron kinetic energy distribution, obtained by measuring the scadered electrons produced by bombardment of Al(lOO) with a 170 eV electron beam. The spectrum shows the elastic peak, loss features due to the excitation of plasmons, a signal due to the emission of Al LMM Auger electrons and the inelastic tail. The exact position of the cutoff at 0 eV depends on die surface work fimction.

See other pages where Surfaces emission distribution is mentioned: [Pg.104]    [Pg.44]    [Pg.37]    [Pg.110]    [Pg.107]    [Pg.288]    [Pg.217]    [Pg.320]    [Pg.141]    [Pg.646]    [Pg.164]    [Pg.189]    [Pg.182]    [Pg.246]    [Pg.303]    [Pg.52]    [Pg.797]    [Pg.184]    [Pg.619]    [Pg.583]    [Pg.351]    [Pg.110]    [Pg.31]    [Pg.267]    [Pg.98]    [Pg.250]    [Pg.65]    [Pg.696]    [Pg.590]    [Pg.313]   
See also in sourсe #XX -- [ Pg.298 , Pg.305 ]




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Emissions distribution

Surface distribution

Surface emission

Surface emissivity

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