Titlebook: Aero- and Hydro-Acoustics; IUTAM Symposium, Eco Geneviève Comte-Bellot,John E. Ffowcs Williams Conference proceedings 1986 Springer-Verlag

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https://doi.org/10.1007/978-1-349-09231-4 the remaining two cases, a vortex ring passes by a sharp edge of a flat plate, its width being comparable with the vortex size for the one case and semi-infini te for the other. This work presents a basis of comparison between the observations and the theoretical predictions.

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Acoustic Waves Emitted by Vortex-Body Interactionthe vortex-body system. In the first case, a vortex ring passes near by a circular cylinder whose axis is set at right angles to the vortex motion. In the remaining two cases, a vortex ring passes by a sharp edge of a flat plate, its width being comparable with the vortex size for the one case and s

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Non-Steady Flow Over a Trailing Edge — An Experimental Studyfield is obtained as close as 0.2 mm away from the wall and we are able to resolve the Stokes layer of the incoming flow. The perturbation of the shear-layer is discussed and the vorticity in the downstream region is evaluated from the velocity field. Additionally the displacement of the separation