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Titlebook: Hands-On Value-at-Risk and Expected Shortfall; A Practical Primer Martin Auer Book 2018 Springer International Publishing AG 2018 Historica

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31#
發(fā)表于 2025-3-27 00:46:05 | 只看該作者
32#
發(fā)表于 2025-3-27 02:20:37 | 只看該作者
perimental data. Both the turbulence model—standard k-? model and Reynolds Stress Model are seen to have their advantages and shortcomings while predicting the local Nusselt number for a particular case of nozzle-to-surface spacing. Analysis of impingement heat transfer using other enhancement techniques awaits further simulation.
33#
發(fā)表于 2025-3-27 06:53:19 | 只看該作者
Martin Auer. It is found that for low Richardson number values, the natural convection mode is dominated by forced convection mode. In addition, increasing the Richardson number leads to a decrease in the rate of heat transfer.
34#
發(fā)表于 2025-3-27 13:15:47 | 只看該作者
Martin Auerocities in the occupied zone are responsible of a slightly cold sensation. The recorded pressure loss is higher in OD than in LD, whereas no significant difference was observed in terms of sound pressure level in the occupied zone.
35#
發(fā)表于 2025-3-27 14:10:52 | 只看該作者
36#
發(fā)表于 2025-3-27 21:40:31 | 只看該作者
Support Measuresely weighs risk factors by both their sensitivity and volatility. Finally, the most helpful measure we take away from the expected shortfall world is the position-wise conditional expected shortfall cES[.|.], which provides a useful complementary breakdown of risk to positions.
37#
發(fā)表于 2025-3-27 22:26:11 | 只看該作者
38#
發(fā)表于 2025-3-28 02:06:10 | 只看該作者
Martin Auer of an incompressible inviscid fluid, two streamline functions are introduced. Any solenoid vector can be presented as a vector product of the gradients of two streamline functions. In order to determine the potential of the velocities, we obtain the relation between the velocity components and the
39#
發(fā)表于 2025-3-28 06:45:44 | 只看該作者
Martin Aueren modeling the special attention is paid to the study of non-stationary flow structure near the lateral surface and bottom regions of the descent module located at different attack angles. The patterns of the non-stationary spatial vortex flow near the descent module are presented. Numerical simula
40#
發(fā)表于 2025-3-28 13:47:48 | 只看該作者
n the impingement regions. This work presents the CFD simulation results of heat transfer characteristics taking into consideration a single turbulent free jet, impinging over a hot flat surface. Effects of different turbulence models, jet turbulent Prandtl number and near wall functions are examine
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