Simulations are reported on the behavior of two tandem symmetric foils in an in-line configuration undergoing pitching motion. The Reynolds number was varied between 1000 and 4000, whereas the pitching Strouhal number ranged from 0.2 to 0.5 and the amplitude of pitching varied from 4 to 8 deg. The streamwise separation distance between the foils was fixed at one chord length. The performance of the downstream foil was significantly worsened (up to 80% in efficiency) by the tandem effects. The Strouhal number, Reynolds number, and pitching amplitude had substantial impact on the performance of the downstream foil. For the upstream foil, however, the performance improved by up to 147% in efficiency at all ranges of Reynolds number, Strouhal n...
In the present paper, a numerical simulation based on Kω-SST turbulence model has been carried out t...
Recently, the problem of a transitional boundary layer around a pitching foil has been attracting in...
The present study is on the experimental investigation of the flow over oscillating NACA4421 airfoil...
The application of tandem flapping foil propulsors to conventional aerial and underwater vehicles pl...
In this study, we present two and three-dimensional numerical investigation to understand the combin...
The propulsive performance of a pair of tandem flapping foils is sensitively dependent on the spacin...
The application of tandem flapping foils propulsors to conventional aerial and underwater vehicles p...
Previous investigations of flapping hydrofoils for the purpose of thrust production have been limite...
###EgeUn###Simulations of symmetrical NACA airfoils pitching about their quarter chord point are pre...
New experiments examine the interactions between a pair of three-dimensional (AR = 2) non-uniformly ...
Two experimental studies are carried out on interacting tandem bodies in incompressible, turbulent f...
The aim of this article is to provide a theoretical basis upon which to advance and deploy novel tan...
The present study is developed within the framework of marine structure design operating in transien...
fluid dynamics videos. The effect of flexibility on the hydrody-namic loads and on the flow structur...
This thesis documents a series of three dimensional unsteady Reynolds Averaged Navier-Stokes CFD sim...
In the present paper, a numerical simulation based on Kω-SST turbulence model has been carried out t...
Recently, the problem of a transitional boundary layer around a pitching foil has been attracting in...
The present study is on the experimental investigation of the flow over oscillating NACA4421 airfoil...
The application of tandem flapping foil propulsors to conventional aerial and underwater vehicles pl...
In this study, we present two and three-dimensional numerical investigation to understand the combin...
The propulsive performance of a pair of tandem flapping foils is sensitively dependent on the spacin...
The application of tandem flapping foils propulsors to conventional aerial and underwater vehicles p...
Previous investigations of flapping hydrofoils for the purpose of thrust production have been limite...
###EgeUn###Simulations of symmetrical NACA airfoils pitching about their quarter chord point are pre...
New experiments examine the interactions between a pair of three-dimensional (AR = 2) non-uniformly ...
Two experimental studies are carried out on interacting tandem bodies in incompressible, turbulent f...
The aim of this article is to provide a theoretical basis upon which to advance and deploy novel tan...
The present study is developed within the framework of marine structure design operating in transien...
fluid dynamics videos. The effect of flexibility on the hydrody-namic loads and on the flow structur...
This thesis documents a series of three dimensional unsteady Reynolds Averaged Navier-Stokes CFD sim...
In the present paper, a numerical simulation based on Kω-SST turbulence model has been carried out t...
Recently, the problem of a transitional boundary layer around a pitching foil has been attracting in...
The present study is on the experimental investigation of the flow over oscillating NACA4421 airfoil...