scholarly journals Optimum aerodynamic design using the Navier-Stokes equations

Author(s):  
A. Jameson ◽  
N. Pierce ◽  
L. Martinelli ◽  
A. Jameson ◽  
N. Pierce ◽  
...  
2003 ◽  
Author(s):  
Andrea Schneider ◽  
Andrea Arnone ◽  
Marco Savelli ◽  
Andrea Ballico ◽  
Paolo Scutellaro

In the last twenty years the theoretical approach to aerodynamic design by means of Computational Fluid Dynamic (CFD) has evolved substantially. The recent improvements in computer performance have made the use of Reynolds Averaged Navier-Stokes equations (RANS) feasible for practical design applications, thereby opening new frontiers in aerodynamic design. RANS codes have broadened the availability of design tools and expanded the design criteria. The latest generation of racing yachts has greatly benefited from the use of these new tools in the design of hulls, appendages and sails. The proposed contribution is focused on the use of RANS in assisting the sail designer. A fully viscous incompressible research code originally developed for aerospace applications has been extended for use in sail plan analysis, thereby allowing the designer to test and compare a large number of sail modifications in a relatively short amount of time. A parametric approach to sail design in upwind conditions will be presented for an America's Cup Yacht. The benefits, weaknesses, and potential of 3D RANS solutions will be discussed in detail.


2020 ◽  
Vol 14 (4) ◽  
pp. 7369-7378
Author(s):  
Ky-Quang Pham ◽  
Xuan-Truong Le ◽  
Cong-Truong Dinh

Splitter blades located between stator blades in a single-stage axial compressor were proposed and investigated in this work to find their effects on aerodynamic performance and operating stability. Aerodynamic performance of the compressor was evaluated using three-dimensional Reynolds-averaged Navier-Stokes equations using the k-e turbulence model with a scalable wall function. The numerical results for the typical performance parameters without stator splitter blades were validated in comparison with experimental data. The numerical results of a parametric study using four geometric parameters (chord length, coverage angle, height and position) of the stator splitter blades showed that the operational stability of the single-stage axial compressor enhances remarkably using the stator splitter blades. The splitters were effective in suppressing flow separation in the stator domain of the compressor at near-stall condition which affects considerably the aerodynamic performance of the compressor.


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