58 research outputs found

    Determining the velocity distribution in the boundary layer of an airfoil fitted with a rotary cylinder

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    In the closer investigation of the results obtained from a wing model with a rotary cylinder mounted in its leading edge (NACA TM's 307 and 354), the velocity distribution in the vicinity of the surface of the model was determined by a hot-wire anemometer. The results confirmed the belief that the rotary cylinder had considerable effect on the air flow, but demonstrated the fact that the direct influence of the cylinder is confined to a very thin layer in immediate proximity to the surface

    Comparison of flow and dispersion properties of free and wall turbulent jets for source dynamics characterisation

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    The objective of this paper is to provide an investigation, using large eddy simulations, into the dispersion of aircraft jets in co-flowing take-off conditions. Before carrying out such study, simple turbulent plane free and wall jet simulations are carried out to validate the computational models and to assess the impact of the presence of the solid boundary on the flow and dispersion properties. The current study represents a step towards a better understanding of the source dynamics behind an airplane jet engine during the take-off and landing phases. The information provided from these simulations can be used for future improvements of existing dispersion models

    Measurements of the velocity distribution in the boundary layer along a plane surface

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    Electrical Engineering, Mathematics and Computer Scienc

    Laminar Flow in Channels with Porous Walls

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    THE VANE ANEMOMETER

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