In the present experimental work, which utilizes a hot-wire visualization method, an influence of external pressure gradient on the development of secondary instabilities in the straight wing boundary layers has been demonstrated for the first time. The comparison of experimental data and direct numerical simulation results of this process has been given. © 2006 Springer.
CITATION STYLE
Kozlov, V. V., Chernoray, V. G., Litvinenko, Y. A., & Löfdahl, L. (2006). Breakdown of a streak via development of varicose secondary mode on the straight wing with pressure gradient. Fluid Mechanics and Its Applications, 78, 419–424. https://doi.org/10.1007/1-4020-4159-4_60
Mendeley helps you to discover research relevant for your work.