Search engine for discovering works of Art, research articles, and books related to Art and Culture
ShareThis
Javascript must be enabled to continue!

Experimental study on aerodynamic characteristics of two tandem square cylinders

View through CrossRef
Abstract Aerodynamic characteristics of two tandem square cylinders are investigated in horizontal and diagonal arrangement respectively, with the variation of the spacing ratio (i.e. the center-to-center space P versus the width B of the square cylinder) P / B  = 1.75–5 at Re  = 8 × 10 4 in the present study. The study focuses on the aerodynamic characteristics of diagonal tandem cylinders and the comparison with those of horizontal tandem cylinders. The results show that the aerodynamic characteristics of two diagonal square cylinders are distinctly different from those in the horizontal arrangement. At the small spacing, the mean and fluctuating aerodynamic coefficients, the maximum of mean negative pressures and the fluctuating pressures for diagonal tandem cylinders are noticeably larger than those of horizontal tandem cylinders due to a pair of recirculation flows. It is interesting that there are multiple peaks in the power spectra of diagonal tandem cylinders. The Strouhal numbers corresponding to the predominate peak of diagonal tandem cylinders are clearly smaller than those of horizontal tandem cylinders at the same spacing ratio. Additionally, the inter- and intra-cylinder correlations of aerodynamic forces for two types of arrangements change diversely with the variation of the spacing ratio. Moreover, the flow modes should be different from those of two horizontal tandem cylinders, which could be concluded to three regions in the investigated spacing ratio.
Title: Experimental study on aerodynamic characteristics of two tandem square cylinders
Description:
Abstract Aerodynamic characteristics of two tandem square cylinders are investigated in horizontal and diagonal arrangement respectively, with the variation of the spacing ratio (i.
e.
the center-to-center space P versus the width B of the square cylinder) P / B  = 1.
75–5 at Re  = 8 × 10 4 in the present study.
The study focuses on the aerodynamic characteristics of diagonal tandem cylinders and the comparison with those of horizontal tandem cylinders.
The results show that the aerodynamic characteristics of two diagonal square cylinders are distinctly different from those in the horizontal arrangement.
At the small spacing, the mean and fluctuating aerodynamic coefficients, the maximum of mean negative pressures and the fluctuating pressures for diagonal tandem cylinders are noticeably larger than those of horizontal tandem cylinders due to a pair of recirculation flows.
It is interesting that there are multiple peaks in the power spectra of diagonal tandem cylinders.
The Strouhal numbers corresponding to the predominate peak of diagonal tandem cylinders are clearly smaller than those of horizontal tandem cylinders at the same spacing ratio.
Additionally, the inter- and intra-cylinder correlations of aerodynamic forces for two types of arrangements change diversely with the variation of the spacing ratio.
Moreover, the flow modes should be different from those of two horizontal tandem cylinders, which could be concluded to three regions in the investigated spacing ratio.

Related Results

Synergistic Flow Induced Oscillation of Multiple Cylinders in Harvesting Marine Hydrokinetic Energy
Synergistic Flow Induced Oscillation of Multiple Cylinders in Harvesting Marine Hydrokinetic Energy
Abstract Flow Induced Oscillations (FIO) of cylinders in tandem can be enhanced by proper spacing to increase hydrokinetic energy harnessing. In a farm of multiple c...
Explainable Aerodynamic Design Framework for Tandem-Wing UAV Based on BO-xRFM
Explainable Aerodynamic Design Framework for Tandem-Wing UAV Based on BO-xRFM
Tandem-wing aircraft boasts broad application prospects in low-speed flight scenarios due to its merits including compact structure, high lift-to-drag ratio and high stability. Nev...
CFD Aerodynamic Analysis of Tandem Tilt-Wing UAVs in Cruise Flight and Tilt Transition Flight
CFD Aerodynamic Analysis of Tandem Tilt-Wing UAVs in Cruise Flight and Tilt Transition Flight
The tandem tilt-wing UAV features an advanced aerodynamic layout design and is regarded as a solution for small-scale urban air mobility. However, the tandem wing configuration exh...
Strouhal Number for VIV Excitation of Long Slender Structures
Strouhal Number for VIV Excitation of Long Slender Structures
The prediction of Vortex-Induced Vibration (VIV) of cylinders under fluid flow conditions depends upon the eddy shedding frequency, conventionally described by the Strouhal Number....
Numerical Investigation on Flow-Induced Vibrations of Circular Sections in Tandem Arrangement Varying Relative Distance
Numerical Investigation on Flow-Induced Vibrations of Circular Sections in Tandem Arrangement Varying Relative Distance
Abstract The flow around a circular section has many applications in engineering, specifically in the offshore area, such as platforms, risers, pipelines, etc. These...
Experimental and computational investigation on interaction between nano rotor and aerodynamic rudder
Experimental and computational investigation on interaction between nano rotor and aerodynamic rudder
The interference effect between the nano rotor and aerodynamic rudder was studied experimentally and computationally. Propulsive performance of nano rotor and aerodynamic performan...
Damage Tolerance and Arrest Characteristics of Pressurized Graphite/Epoxy Tape Cylinders
Damage Tolerance and Arrest Characteristics of Pressurized Graphite/Epoxy Tape Cylinders
An investigation of the damage tolerance and damage arrest characteristics of internally pressurized graphite/epoxy tape cylinders with axial notches was conducted. An existing fai...
Applications
Applications
ExCALIBUR Project NEPTUNE: Nektar++ for fusion plasma simulationProject NEPTUNE (NEutrals and Plasma Turbulence Numerics for the Exascale; part of the UK's ExCALIBUR programme) aim...

Back to Top