Publicou 4 edições por ano
ISSN On-line: 2152-209X
INSTABILITY OF A SWEPT-WING BOUNDARY LAYER MODULATED BY STATIONARY FLOW PERTURBATIONS
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.
-
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
-
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