Results 11 to 20 of about 62,591 (316)
Open Physics, 2022 This article aims to conduct a numerical investigation of phenomena induced by gas expansion in chemical propulsion nozzles. A numerical simulation of full-scale flat convergent-divergent nozzle geometry using the finite volume method on structured ...
Dehane Rabie +6 more
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Vietnam Journal of Mechanics, 2011 For compressible flows, the transonic state depends on the geometry, Mach number and the incidence. This effect can produce shock wave. Some studies showed that the interaction between shock wave and boundary layer concerns separation phenomenon. Studies
Hoang Thi Bich Ngoc, Nguyen Manh Hung
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Numerical study of the effect of sidewalls on shock train behaviour
Flow, 2023 Strongly coupled sequences of shock waves, known as shock trains, are present in high-speed propulsion systems, where the presence of sidewalls substantially modifies the boundary layer thickness, skin friction and streamwise pressure distribution.
Alexander Gillespie, Neil D. Sandham
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Direct numerical simulation of 'short' laminar separation bubbles with turbulent reattachment [PDF]
, 2000 Direct numerical simulation of the incompressible Navier–Stokes equations is used to study flows where laminar boundary-layer separation is followed by turbulent reattachment forming a closed region known as a laminar separation bubble.
Alam, M., Sandham, N.D.
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Active Boundary Layer Control on a Highly Loaded Turbine Exit Case Profile
International Journal of Turbomachinery, Propulsion and Power, 2018 A highly loaded turbine exit guide vane with active boundary layer control was investigated experimentally in the High Speed Cascade Wind Tunnel at the University of the German Federal Armed Forces, Munich.
Julia Kurz +2 more
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Advances in Mechanical Engineering, 2019 At hypersonic speeds, the external wall temperatures of an aerospace vehicle vary significantly. As a result, there is a considerable heat transfer variation between the boundary layer and the wall of the hypersonic vehicle.
Amjad A Pasha, Khalid A Juhany
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Investigation into boundary layer transition using wall-resolved large-eddy simulations and modeled inflow turbulence [PDF]
Wind Energy Science, 2022 The objective of the present paper is to investigate the transition scenario of the flow around a typical section of a wind turbine blade exposed to different levels of inflow turbulence.
B. A. Lobo +2 more
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Entrainment and boundary-layer separation: a modeling history [PDF]
Journal of Engineering Mathematics, 2017 zbMATH Open Web Interface contents unavailable due to conflicting licenses.
openaire +2 more sources
Implementation of a correction factor for the Pohlhausen laminar boundary layer applied on the CEVA curved wall jet model [PDF]
INCAS Bulletin, 2013 Curved wall jets have many technical applications, ranging from aeronautical circulation controlled wings to micro-fluidics and cryogenics. This paper addresses the issue of correctly estimating the boundary layer separation for laminar curved wall jets.
Valeriu DRAGAN
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The flow structure behind vortex generators embedded in a decelerating turbulent boundary layer [PDF]
, 2009 The objective of the present work is to analyse the behaviour of a turbulent decelerating boundary layer under the effect of both passive and active jets vortex generators (VGs).
Braud, Caroline +3 more
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