Results 11 to 20 of about 1,835,674 (303)
Wave Response of a Monocolumn Platform with a Skirt Using CFD and Experimental Approaches
Journal of Marine Science and Engineering, 2022 This paper aims to investigate the nonlinear motion characteristics of a monocolumn type floater with skirts numerically and experimentally. Wave calibration, free decay, and regular wave tests were simulated using a computational fluid dynamics (CFD ...
Masaki Katafuchi +5 more
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Numerical Investigation on Flow Separation Control of Low Reynolds Number Sinusoidal Aerofoils [PDF]
, 2016 The paper presents a computational analysis of the characteristics of a NACA 634- 021 aerofoil incorporated with sinusoidal leading-edge protuberances at Re = 14,000. The protuberances are characterized by an amplitude and wavelength of 12% and 50% of
Cai C. +4 more
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Effects of Plasma Actuator Discharge on Lift-Enhancement and Flow Patterns of Flying Wing Aircraft [PDF]
Xibei Gongye Daxue Xuebao, 2018 The nanosecond pulsed plasma discharge actuator is used on a flying wing aircraft. At the angles of attack rang from -4° to 28°, the impact of plasma actuator arrangement position and discharge frequency on lift-enhancement effect is tested.
doaj +1 more source
Mathematics, 2022 Thermal performance and phase-change dynamics in a channel having a cavity equipped with a heater and phase-change material (PCM)-packed bed (PB) region are analyzed during nanoliquid convection under an inclined magnetic field.
Walid Aich +5 more
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Structure and Topology Analysis of Separated Vortex in Forward-Swept Blade
Frontiers in Energy Research, 2021 Flow separation commonly affects the stability of turbomachines, especially under low-flowrate conditions. Compared with conventional blades, a forward-swept blade is more efficient at high flowrates.
D. Liang +4 more
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Heat Induced Separation in Upward Impinging Jet Flows
Journal of Thermal Science and Technology, 2011 A confined, round, laminar impinging jet, fed upward against the gravity, is studied, both experimentally and numerically, under the influence of an impingement-surface heating.
Chandra SHEKHAR, Koichi NISHINO
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Journal of Fluid Science and Technology, 2010 Direct numerical simulations (DNS) of turbulent flow through an asymmetric plane diffuser, consisting of a flat wall and an inclined wall, were performed using a high-order finite difference method, to reveal the relationship between turbulence and flow ...
Takashi OHTA, Takeo KAJISHIMA
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Numerical Study of Stream-wise and Span-wise Nanosecond DBD Plasma Actuators Effects on Supersonic Flow Separation [PDF]
Journal of Applied Fluid Mechanics, 2022 The current paper aimed to investigate the primary control mechanism of various Nanosecond Dielectric Barrier Discharge (NS-DBD) plasma actuators on the Shock Wave/Boundary Layer Interaction (SWBLI).
A. Nazarian Shahrbabaki +2 more
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Increasing L/D Ratio of Wing by Delaying Flow Separation for Better Aerodynamic Performance [PDF]
Journal of Applied Fluid MechanicsTo improve the aerodynamic efficiency of the aircraft, the article focuses on optimizing the L/D ratio through postponement of flow separation. Elevating the L/D ratio leads to diminished drag and delays stall occurrence at high angles of attack (α). The
L. P. Ramesh, V. Mugendiran, G. Sivaraj
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Global stability of separated flows: Subsonic flow past corners: F separated flows
Theoretical and Computational Fluid Dynamics, 2011 The triple-deck equations for the steady subsonic flow past a convex corner are solved numerically using a novel technique based on Chebychev collocation in the direction normal to the body combined with finite differences in the direction along the flow.
Logue, R. P. +2 more
openaire +2 more sources