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main units including the drop generator, the impact substrate and the

...atomizer main axis was 150 mm away from the section inlet and crossed the main section axis. Positioning of the atomizer relative to the section (7) is sh ...der with a diameter of 45 mm and 27 mm long with its axis identical to the main atomizer axis, see '''[https://kbwiki.ercoftac.org/w/index.php/EXP_1-1_Meas

...ogether the expertise of 43 participating organisations across Europe. The main objective of the Network was to improve the level of trust that can be plac

...rynx and the upper trachea were imaged by plane V, and plane VI covers the main bifurcation and bronchi. ...>2^o</math> from the exact vertical orientation), trachea (V-xy plane) and main bifurcation and bronchi (VI-yz plane).]]

...lly, a protuberance was attached at the intersection of the collateral and main branch to mimic blood flow patterns in an aortic aneurysm (Fig. 2). Typical ...ath> is the averaged inlet velocity and <math>D</math> the diameter of the main duct. At peak systole (highest inlet velocity), a maximum <math>Re = 1915</

...ed. The Mach number distribution right in front of the leading edge of the main blade (plane -1) is presented in Fig. 4.1, the Mach number distribution at ...al computational domain is limited to a single rotating passage (including main blade and splitter blade flow), because the geometrical simplifications and

...locate the junction at least 1000 mm downstream of the nearest bend of the main pipe (no precise measurements have been made to assess the development of t ! || Inlet Re ||width="100"| Main Pipe Bulk Velocity (m/s) ||width="100"|Auxiliary Pipe Bulk Velocity (m/s) |

=== Main Assessment Quantities === Considering the experimental data available the main assessment quantities are time histories (hysteresis) of Cl(t) &mdash; lift

At planes VI (main bifurcation and bronchi, see [[Test Data AC7-02#Figure6|figure 6]](b)), the At planes VI (main bifurcation and bronchi, see [[Test Data AC7-02#Figure6|figure 6]](b)), the

...and the bluff-body jet flames discussed here consist, generally, of three main zones: stabilization, extinction and reignition zones. The computation of t ...ownstream towards the outlet section. Beside the downstream motion of this main recirculation vortex, a new one starts to develop at the bluff-body wall re

...dation of numerical methodologies. This flow has been considered, with the main objective of assessment of turbulence models, during the E.C. funded projec

could also capture most of the main features of the complex flow, including the vortex One of the main uncertainties is the oncoming boundary layer developing on the ground plate

(i) a main hydraulic circuit, marked blue; (iv) a main pump that is able to provide a maximum flow rate of 40 l/s;

Transition was set on the main element lower and upper surfaces at 12.5% retracted chord. • Surface pressure coefficients on the slat, main-element and flap

Three main flow patterns are potential sources of losses in turbomachinery. These are: ...by the interaction of the pressure gradient linked to the curvature of the main flow with the non-uniform flow (for instance due to boundary layers on soli

...d tunnel NWG in Göttingen. The model shape is defined analytically and the main dimensions are the following: ...eroid has been simulated during the E.C. funded project ECARP [8] with the main purpose of validation of the turbulence models. The flow conditions chosen

The flow domain geometry is shown in [[#Fig. 1|Fig. 1]]. Only the main river channel with groynes is included but not the flood plains which remai ...ure was 14&deg;C. At the discharge considered the flow is contained in the main river channel and the groynes are only slightly submerged so that there are

Margason (1993) gives a list of the main applications of knowledge about jets in cross flow: ...he case of R=0.5. The jet bends immediately after leaving the orifice. The main flow is slightly distorted by the jet and, downstream the orifice, it looks

...ar in plan, with an aerofoil-shaped roof. It is located near to one of the main runways of the airport. The surrounding area is relatively open, with a few ...be evaluated. This is an unusual requirement for building design, and the main parameters that were assessed were the velocity defect and turbulence enhan

Schematic view on the main and pilot burners located 15 cm above the |Main jet inner diameter, ''d''||=||7.2 mm