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NASA NTRS · 19780061667

The free shear layer tone phenomenon and probe interference

Abstract

The reported investigation shows that the hot-wire probe induces stable upstream oscillations in a free shear layer, similar to the jet edge tone mechanism. This effect can be significant also in measurements involving large-scale organized structure, conditional sampling, space-time correlation, and convection velocity, when a reference or indicator probe may be used near the origin of the free shear layer. It appears that even in a free shear layer without any wedge, an object in the flow sufficiently downstream can also provide feedback to the flow upstream. A description is given of the edge-tone phenomenon which is observed when a thin slit jet impinges on a plane wedge. Attention is given to the free shear layer tone induced by a hot-wire probe, the free shear layer tone phenomenon, and shear layer tone eigenvalues and eigenfunctions.

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BibTeXRIS

Hussain, A. K. M. F., Zaman, K. B. M. Q.. 1978-07-26. The free shear layer tone phenomenon and probe interference. https://ntrs.nasa.gov/citations/19780061667

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