scholarly journals Optimum aerodynamic design for wind-lens turbine

2016 ◽  
Vol 11 (2) ◽  
pp. JFST0011-JFST0011 ◽  
Author(s):  
Nobuhito OKA ◽  
Masato FURUKAWA ◽  
Kenta KAWAMITSU ◽  
Kazutoyo YAMADA
1997 ◽  
Author(s):  
A. Jameson ◽  
N. Pierce ◽  
L. Martinelli ◽  
A. Jameson ◽  
N. Pierce ◽  
...  

Author(s):  
A N M Mominul Islam Mukut ◽  
Mohammad Zoynal Abedin

Due to higher price, limited supply and negative impacts on environment by fossil fuel, automobile industries have directed their concentrations in reducing the fuel consumption of vehicles in order to achieve the lower aerodynamic drag. As a consequence, numerous researches have been carried out throughout the world for not only getting the optimum aerodynamic design with lower drag penalty and but also other parameters that increases the fuel consumption. In this regard, relevant experimental and numerical outcomes on vehicle drag reduction considering various techniques such as active, passive and combined techniques in order to delay or suppress flow separation behind the vehicles have been considered in this review paper. Furthermore, the effects of drag reduction and their applicability on the vehicles are also illustrated in this paper. Therefore, it is conjectured that the drag reduction has been improved as much as 20%, 21.2%, and 30% by using the active, passive and combined control systems, respectively.


AIAA Journal ◽  
1976 ◽  
Vol 14 (11) ◽  
pp. 1524-1527 ◽  
Author(s):  
H.J. Stewart

Author(s):  
Nobuhito Oka ◽  
Masato Furukawa ◽  
Kazutoyo Yamada ◽  
Sasuga Itou ◽  
Seiichi Ibaraki ◽  
...  

An optimum aerodynamic design method for centrifugal compressor impeller has been developed. The present optimum design method is using a genetic algorithm (GA) and a two-dimensional inverse blade design method based on a meridional viscous flow analysis. In the meridional viscous flow analysis, an axisymmetric viscous flow is numerically analyzed on a two-dimensional meridional grid to determine the flow distribution around the impeller. Full and splitter blade effects to the flow field are successfully evaluated in the meridional viscous flow analysis by a blade force modeling. In the inverse blade design procedure, blade loading distribution is given as the design variable. In the optimization procedure, the total pressure rise and adiabatic efficiency obtained from the meridional viscous flow analysis are employed as objective functions. Aerodynamic performance and three-dimensional flow fields in the Pareto-optimum design and conventional design cases have been investigated by three-dimensional Reynolds averaged Navier-Stokes (3D-RANS) and experimental analyses. The analyses results show performance improvements and suppressions of flow separations on the suction surfaces in the optimum design cases. Therefore, the present aerodynamic optimization using the inverse method based on the meridional viscous flow analysis is successfully achieved.


2013 ◽  
Vol 55 ◽  
pp. 296-304 ◽  
Author(s):  
Déborah Aline Tavares Dias do Rio Vaz ◽  
Jerson Rogério Pinheiro Vaz ◽  
André Luiz Amarante Mesquita ◽  
João Tavares Pinho ◽  
Antonio Cesar Pinho Brasil Junior

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