On the breakdown of boundary layer streaks
Web1 de jan. de 2007 · When the jet velocity is low, some vortices appear in the boundary layer, but the transition of the boundary layer does not take place. However, when the … WebDOI: 10.2514/1.j062638 Corpus ID: 257904225; Groove Coating's Effect on Linear and Nonlinear Instability of High-Speed Boundary Layer @article{Zhou2024GrooveCE, title={Groove Coating's Effect on Linear and Nonlinear Instability of High-Speed Boundary Layer}, author={Teng Zhou and Zaijie Liu and Chao Yan}, journal={AIAA Journal}, …
On the breakdown of boundary layer streaks
Did you know?
Web1 de abr. de 2024 · [3] Franko K. and Lele S., “ Breakdown Mechanisms and Heat Transfer Overshoot in Hypersonic Zero Pressure Gradient Boundary Layers,” Journal of Fluid Mechanics, Vol. 730, Sept. 2013, pp. 491–532. Web18 de set. de 2013 · The stability theory is robust, and can predict the particular streaks which are likely to undergo secondary instability and break down in transitional …
Web18 de set. de 2013 · Douglas Hofstadter Bypass transition to turbulence in boundary layers is examined using linear theory and direct numerical ... On the breakdown of boundary layer streaks. J. Fluid Mech. 428, 29–60 (2001) Article MathSciNet MATH Google Scholar Barkley, D., Blackburn, H.M., Sherwin, S.J.: Direct optimal growth analysis for ... WebPaper 1. On the breakdown of boundary layer streaks 51 Paper 2. On the convectively unstable nature of optimal streaks in boundary layers 93 Paper 3. Transition of streamwise streaks in zero-pressure-gradient boundary layers 123 Paper 4. Stabilization of Tollmien-Schlichting waves by nite amplitude optimal streaks in the Blasius boundary layer ...
WebNumerical simulations of bypass transition in Blasius boundary layers are presented. The breakdown of streamwise streaks is first considered in the case of the steady, spanwise periodic basic flows arising from the nonlinear saturation of optimal perturbations and then in the case of transition in boundary layers subject to free-stream turbulence. Web2 de ago. de 2016 · On the breakdown of boundary layer streaks. J. Fluid Mech. 428, 29–60 (2001) Article MATH MathSciNet Google Scholar Bagheri, S., Hanifi, A.: The stabilizing effect of streaks on ... Talamelli, A.: On the generation of steady streamwise streaks in flat-plate boundary layers. J. Fluid Mech. 698, 211–234 (2012)
WebNumerical simulations of bypass transition in Blasius boundary layers are presented. The breakdown of streamwise streaks is first considered in the case of the steady, spanwise …
Web7 de abr. de 2024 · Görtler vortex-induced hypersonic boundary layer transition controlled by grooves is investigated using direct numerical simulations and spatial bi-global stability analysis. ... sinuous mode S1 also covers a larger frequency range than the other two secondary instability modes and results in the breakdown of Görtler streaks. greensboro nc fair market rentWeb13 de fev. de 2001 · Experimental and theoretical investigation of the nonmodal growth of steady streaks in a flat plate boundary layer. Physics of Fluids, Vol. 16, Issue. 10, p. 3627. CrossRef greensboro nc family ymcaWeb©2007 The Visualization Society of Japan Journal of Visualization, Vol. 10, No. 2 (2007)217-225 Influence of an Unfavourable Pressure Gradient on the Breakdown of Boundary Layer Streaks Chernoray, V. G.*1, Kozlov, V. V.*2, Lee, I.*3 and Chun, H. H.*3 *1 Applied Mechanics, Chalmers University of Technology, SE-412 96, Gothenburg, Sweden. *2 … greensboro nc fall festivalsWeb8 de abr. de 2024 · In conclusion, grooves can delay Gortler vortex-induced transition by modifying the Gortler streaks structure and instability, which would shed light on hypersonic boundary layer transition control. fmb outlookWebDOI: 10.2514/1.j062638 Corpus ID: 257904225; Groove Coating's Effect on Linear and Nonlinear Instability of High-Speed Boundary Layer @article{Zhou2024GrooveCE, … greensboro nc fboWeb30 de mai. de 2024 · In this study direct numerical simulation is employed to investigate the effects of various parameters on the flow control capabilities of narrowly spaced streaks in a boundary layer at M ∞ = 2.0. greensboro nc fairWeb4 de ago. de 2005 · The linear perturbations evolving on streamwise boundary layer streaks which yield maximum energy growth are computed. The steady and spanwise … fmbphh