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Visualization of Mechanical Processes: An International Online Journal

Publicou 4 edições por ano

ISSN On-line: 2152-209X

INSTABILITY OF A SWEPT-WING BOUNDARY LAYER MODULATED BY STATIONARY FLOW PERTURBATIONS

Volume 3, Edição 1, 2013,
DOI: 10.1615/VisMechProc.2013006967
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RESUMO

A collection of illustrations of swept-wing boundary layer secondary instability at low subsonic flow velocities is presented in this paper. The experimental results, obtained by hot-wire "visualization," provide detailed insight into the spatio-temporal structure and evolution of oscillations in the three-dimensional laminar boundary layer disturbed by longitudinal vortices and streaky structures.

CITADO POR
  1. Sorokin A. M., Grek G. R., Gilev V. M., Zverkov I. D., Creation of subsonic macro-and microjets facilities and automated measuring system (AMS-2) for the spatial – temporal hot – wire anemometric visualization of jet flow field, 1893, 2017. Crossref

  2. Sorokin A. M., Grek G. R., Gilev V. M., Litvinenko Yu. A., Application of the automated measuring complex (AMC 2) in an aerodynamic experiment, 2027, 2018. Crossref

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