Exact(1)
The model has been compared with the experimental data obtained with both a heated-grid reactor and an entrained-flow reactor to recover the major parameters of the model, i.e. the transition and exit intensity functions.
Similar(59)
There is a substantial difference between the exit wave intensities.
The generalized sourced multi-flux method (GSMFM) is applied to simulate the exit radiation intensities in arbitrary directions at the boundary surfaces of absorbing, emitting, and scattering media, which are used as inputs for the inverse analysis.
Furthermore, increasing the intensity of exit sign takes only effect in some extent.
By determining the relationship between mean first-exit time and noise intensity, it is found that each attractor can be characterized by an activation energy which yields a measure of its relative stability.
To increase the contrast, it is necessary to change the phase of the scattered beam φpr(r⃗) by 90°, which changes the exit wave as follows: The intensity in the image plane then can be approximated by the following expression: Here, the intensity becomes proportional to the projection of the electron potential of the sample, and the magnitude of 2σφpr(r⃗) will be much greater than (σφpr(r⃗)).
Here a 1-D Mythen detector was used to resolve the diffracted intensity along the exit angle.
For a particular focus setting, the intensity of the exit wave function is displayed in Fig. 2c together with the various propagation intensities in beam direction.
As the mean nozzle exit velocity and the turbulence intensity are increased to bring the flame nearer to extinction, the individual flame brushes thicken as much as 50%.
When these physical phenomena are convoluted with the residence time distribution characterizing a WSR (simulating, say, the primary zone of an aircraft gas turbine combustor), we predict the resulting fraction evaporated, evaporation rate-controlled combustion "intensity", and corresponding exit droplet size distributions (DSD).
Effect of velocity profile and turbulence intensity at jet exit on jet entrainment are examined based on the field synergy theory by calculating the mass transfer field synergy number, that is the synergy between the velocity vectors and the species concentration gradients for a given jet flow rate.
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