2003
DOI: 10.7551/mitpress/6781.001.0001
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The Theory of Turbulent Jets

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Cited by 198 publications
(294 citation statements)
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“…The need for reliable wake modelling has been recognized for many years, and various models have been developed to simulate the W/T wakes. Many of them are simple kinematic models based on self‐similar velocity deficit profiles obtained from experimental and theoretical work on mixing jets 1–3. A more advanced approach is that of the field (or implicit) models that calculate the flow quantities at every point of the flow field giving a better insight into the physical mechanisms that govern the wake development.…”
Section: Introductionmentioning
confidence: 99%
“…The need for reliable wake modelling has been recognized for many years, and various models have been developed to simulate the W/T wakes. Many of them are simple kinematic models based on self‐similar velocity deficit profiles obtained from experimental and theoretical work on mixing jets 1–3. A more advanced approach is that of the field (or implicit) models that calculate the flow quantities at every point of the flow field giving a better insight into the physical mechanisms that govern the wake development.…”
Section: Introductionmentioning
confidence: 99%
“…When the standoff distance and nozzle diameter are settled, the velocity within jet range radially decreases away from the center line, which can be described as a bell‐shaped profile. Further, the velocity distribution on each of jet cross section can be expressed by characteristic variables of velocity and scaled into the same mathematical model as shown in Equation , namely the self‐similarity of jet velocity distribution . The results of ground test (see Figure ) showed the core impacting length of waterjet has a linear increase with jet velocity.…”
Section: Resultsmentioning
confidence: 99%
“…( ) is density of water and air mixture at actual distance; S is cross section of nozzle; x is distance; r is radius of nozzle. Figure 9 shows schematic velocity profile calculated by (12) applied on surfaces of profile in the FEM analysis [8,9] All of these ingredients were implemented in our in-house massively parallel code ESPRESO, which is a massively parallel framework based on the finite element method for engineering application. The free license for the developed package allows automatized simulation chains such as automatized systems for optimization to be created above the "solver as a service" platform.…”
Section: Fem Simulationmentioning
confidence: 99%