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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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perimental data. Both the turbulence model—standard k-ɛ 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.
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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.
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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.
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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.
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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
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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
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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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