Results 21 to 30 of about 454,024 (311)
Decomposition Methods For a Piv Data Analysis with Application to a Boundary Layer Separation Dynamics [PDF]
Separation of the turbulent boundary layer (BL) on a flat plate under adverse pressure gradient was studied experimentally using Time-Resolved PIV technique. The results of spatio-temporal analysis of flow-field in the separation zone are presented. For
Václav URUBA
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Entrainment and boundary-layer separation: a modeling history [PDF]
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
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Investigation of turbulence models with compressibility corrections for hypersonic boundary flows
The applications of pressure work, pressure-dilatation, and dilatation-dissipation (Sarkar, Zeman, and Wilcox) models to hypersonic boundary flows are investigated.
Han Tang, Zhenxun Gao
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The objective of this paper is to numerically study the shock wave/boundary layer interaction and boundary layer separation. The first stage of this research is the development of methodology, flow simulations, and data analysis. When comparing the plots,
Ana Maria Pereira Lara +1 more
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Closed-loop separation control over a sharp edge ramp using Genetic Programming [PDF]
We experimentally perform open and closed-loop control of a separating turbulent boundary layer downstream from a sharp edge ramp. The turbulent boundary layer just above the separation point has a Reynolds number $Re_{\theta}\approx 3\,500$ based on ...
A Seifert +37 more
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Numerical Analysis of Effect of Boundary Layer Characteristics on the Flow Field in S-shaped Inlet
In order to explore the effect of boundary layer thickness and pressure gradient on the performance of the flow field in the inlet, we design a high offset rate S-shaped inlet based on a certain unmanned aerial vehicle (UAV), and its author has analyzed ...
Ren Jia +4 more
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Experimental Study on Time Evolution of Shock Wave and Turbulent Boundary Layer Interactions
In this paper, a test system based on the Nano-tracer Planar Laser Scattering (NPLS) technique for studying time evolution of unsteady flow structures was finished.
X. G. Lu +4 more
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This study numerically explores the flow physics associated with nanosecond pulsed plasma actuators to control shock-wave induced boundary-layer separation.
Kinefuchi, Kiyoshi +2 more
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Unsteady separation in vortex-induced boundary layers [PDF]
This paper provides a brief review of the analytical and numerical developments related to unsteady boundary-layer separation, in particular as it relates to vortex-induced flows, leading up to our present understanding of this important feature in high-Reynolds-number, surface-bounded flows in the presence of an adverse pressure gradient.
Cassel, K. W., Conlisk, A. T.
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The Study of Different Fairings for Fairing and Drag Reduction on theLow-wing Layout Aircraft
For the low-wing configuration aircraft, server flow interference exist at the wing-body junction, the boundary layer stack at the junction is the main reason for flow separation, the flow separation results in drag addition.
Zhang Li, Gao Zhenghong
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