Results 11 to 20 of about 8,671,015 (345)
This paper shows the results of an experimental investigation into the effect of changes in solidity on the performance of a Vertical Axis Wind Turbine.
O. Eboibi, L. A. Danao, R. Howell
semanticscholar +3 more sources
Convergence of transonic wind tunnel test results of the AGARD-B standard model [PDF]
AGARD-B is a widely-used configuration of a standard wind tunnel model. Beside its originally intended application for correlation of data from supersonic wind tunnel facilities, it was tested in a wide range of Mach numbers and, more recently, used for ...
Damljanović Dijana +3 more
doaj
Sand transverse dune aerodynamics: 3D Coherent Flow Structures from a computational study [PDF]
The engineering interest about dune fields is dictated by the their interaction with a number of human infrastructures in arid environments. Sand dunes dynamics is dictated by wind and its ability to induce sand erosion, transport and deposition.
Bruno, Luca, Fransos, Davide
core +2 more sources
Unsteady flow behaviour of multi-rotors in ground proximity
The unsteady flow behaviour of two side-by-side rotors in ground proximity is experimentally investigated. The rotors induce a velocity distribution interacting with the ground causing the radial expansion of the rotor wakes.
Hasse N.J. Dekker +4 more
doaj +1 more source
Buildings are bluff bodies, compared to streamline objects, such as airfoil. Wind flow over buildings leads to separation and hence a complex spatial and temporal mechanism that governs the nature and intensity of aerodynamic forces.
A. Aly, F. Khaled, H. Gol-Zaroudi
semanticscholar +1 more source
Experimental Investigation of the Cooperation of Wind Turbines
The article discusses the wind tunnel experimental investigation of two turbines (the downstream unit placed fully in the wake of the upstream one) at various turbulence intensity levels and wind turbine separation distances, at a Reynolds number of ...
Piotr Wiklak +3 more
doaj +1 more source
The shock wave boundary layer interaction on the suction side of a transonic compressor blade is one of the main objectives of the TFAST project (Transition Location Effect on Shock Wave Boundary Layer Interaction).
MICHAŁ PIOTROWICZ +2 more
doaj +1 more source
Aerodynamic Investigation of a Morphing Wing for Micro Air Vehicle by Means of PIV
A wind tunnel tests campaign has been conducted to investigate the aerodynamic flow around a wing morphing to be used in a micro air vehicle. Non-intrusive whole field measurements were obtained by using PIV, in order to compare the velocity and ...
Rafael Bardera +2 more
doaj +1 more source
This paper deals with the estimation of propulsive effects for a three-lifting surface turboprop aircraft concept, with rear engine installation at the horizontal tail tips, conceived to carry up to 130 passengers.
Salvatore Corcione +3 more
doaj +1 more source

