Verification of Turbulence Models for Flow in a Constricted Pipe at Low\n Reynolds Number [PDF]
Fardin Khalili +2 more
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Automated Process Optimization in a Novel Triple Shaft Mixer with Adaptive Mixing Modes
A novel multi‐purpose mixer with adjustable blade angle and a coaxial stirrer is developed, providing three degrees of freedom. An optimization strategy is integrated to autonomously identify optimal operating conditions through automated tests. The current draw of the main stirrer serves as the optimization criterion, while stirrer speeds, directions,
B. Schwarz, H. Kniele, J. A. Lindner
wiley +1 more source
Numerical study of separation on the trailing edge of a symmetrical airfoil at a low Reynolds number
Juanmian Lei, Feng Guo, Can Huang
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Two-dimensional energy spectra in high-Reynolds-number turbulent boundary layers [PDF]
Dileep Chandran +3 more
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Optimal model‐based design of experiments for parameter precision: Supercritical extraction case
Abstract This study investigates the process of chamomile oil extraction from flowers. A parameter‐distributed model consisting of a set of partial differential equations is used to describe the governing mass transfer phenomena in a cylindrical packed bed with solid chamomile particles under supercritical conditions using carbon dioxide as a solvent ...
Oliwer Sliczniuk, Pekka Oinas
wiley +1 more source
E16 Self-Induced Oscillation of a Low Reynolds Number Jet in Fluidic Oscillators
Keita TSUKAHARA, Toru KOSO
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ABSTRACT Septins are conserved GTP‐binding proteins that play key roles in cell division, mitochondrial dynamics and immune responses. Despite their importance to human health, pharmacological compounds to modify septins remain limited. Forchlorfenuron (FCF) was the first small molecule identified to modify septins, disrupting their organisation and ...
Dominik Brokatzky +4 more
wiley +1 more source
Modeling of Pitching and Plunging Airfoils at Reynolds Number between 1x10^4 and 6x10^4
Chang-kwon Kang +7 more
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Closure to “Discussion of ‘Friction Drag on Bladed Disks in Housings as a Function of Reynolds Number, Axial and Radial Clearance, and Blade Aspect Ratio and Solidity’” (1961, ASME J. Basic Eng., 83, p. 723) [PDF]
Robert W. Mann, C. H. Marston
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A Navier-Stokes code, developed by N.L. Sankar, and an Interactive Boundary Layer code, developed by Tuncer Cebeci, are implemented for high Reynolds number, low Mach flows over a NACA 0012 airfoil. Upper surface pressure distributions, coefficients of lift, coefficients of friction, and velocity profiles obtained from the Navier-Stokes code are ...
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