1973
DOI: 10.13182/nt73-a31250
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Pressure Drop Correlations for Fuel Element Spacers

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Cited by 279 publications
(73 citation statements)
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“…Here, V is the velocity, v the kinetic viscosity. Figure 2 displays that K is strongly dependent on the ratio of flow areas A 2 /A 1 and the length of a spacer, as described by Rehme (8) and Okubo, et al (10) When A 2 /A 1 is between 0.7 and 0.8, K ranges from 0.5 to 1.0. The K value is usually adopted in the pressure loss calculation of the reactor core with multi-rod fuel bundles.…”
Section: Friction Loss At Tight-lattice Configurationmentioning
confidence: 74%
See 1 more Smart Citation
“…Here, V is the velocity, v the kinetic viscosity. Figure 2 displays that K is strongly dependent on the ratio of flow areas A 2 /A 1 and the length of a spacer, as described by Rehme (8) and Okubo, et al (10) When A 2 /A 1 is between 0.7 and 0.8, K ranges from 0.5 to 1.0. The K value is usually adopted in the pressure loss calculation of the reactor core with multi-rod fuel bundles.…”
Section: Friction Loss At Tight-lattice Configurationmentioning
confidence: 74%
“…A simple evaluation method for the spacer loss is therefore useful for the design of the reactor cores with the multi-rod bundles. Rehme (8) investigated the pressure loss at the several types of spacers experimentally. He indicated that the loss coefficient for the grid-type spacers is dependent on the relative plugging of a flow cross section, whereas the pressure loss coefficient for the wire-wrapped rod bundle is dependent on the lead of wire wraps.…”
Section: Friction Loss At Tight-lattice Configurationmentioning
confidence: 99%
“…The spacer pressure drop can be comparable in magnitude to the friction along the bare rod bundle. Rehme [7] has undertaken several studies to determine the pressure drop across spacers with different geometries. After detailed experiments, Rehme devised a list of pressure drop coefficients across the spacers with different geometries and with different arrangements.…”
Section: Pressure Drop Across Spacersmentioning
confidence: 99%
“…The drag force on the grid region is divided into four parts: form drag on the grid, frictional drag on the grid, frictional drag on t,he rod, and form drag on the mixing vanc: F = FEE + F::: + FE: + FEZ"'. (1) A grid loss coefficient is defined, for practical use, on the free flow area of bare rod region A0 as follws: But actually t,he pressure drop at grid region may be governed by the flow velocity at grid. In the present model each pressure drop A P is determined on the average velocity at grid region Us, and formulated by introducing the available form or frictional loss coefficienh from t,he open literatures.…”
Section: A Proposed Modelmentioning
confidence: 99%