Improvement of the flow around airfoil/flat-plate junctures by optimization of the leading-edge fence
暂无分享,去创建一个
[1] Om P. Sharma,et al. Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades , 1986 .
[2] D. Clarke,et al. Simulation of a Wing-Body Junction Experiment Using the Fluent Code , 2005 .
[3] Johann Sienz,et al. Formulation of the Optimal Latin Hypercube Design of Experiments Using a Permutation Genetic Algorithm , 2004 .
[4] S. Orszag,et al. Renormalization group analysis of turbulence. I. Basic theory , 1986 .
[5] Lee S. Langston,et al. Horseshoe Vortex Formation Around a Cylinder , 1986 .
[6] D. G. Gregory-Smith,et al. Turbulence Measurements and Secondary Flows in a Turbine Rotor Cascade , 1988 .
[7] W. D. Harvey,et al. Juncture flow control using leading-edge fillets , 1985 .
[8] Douglas C. Montgomery,et al. Response Surface Methodology: Process and Product Optimization Using Designed Experiments , 1995 .
[9] William J. Devenport,et al. Effects of a leading-edge fillet on the flow past an appendage-body junction , 1992 .
[10] Leslie M. Smith,et al. Renormalization group analysis of turbulence , 2003 .
[11] Karen A. Thole,et al. Computational Design and Experimental Evaluation of Using a Leading Edge Fillet on a Gas Turbine Vane , 2001 .
[12] Les A. Piegl,et al. The NURBS Book , 1995, Monographs in Visual Communication.
[13] SemIh M. Ölçmen,et al. An experimental study of a three-dimensional pressure-driven turbulent boundary layer , 1995 .
[14] Roger L. Simpson,et al. Some features of a turbulent wing-body junction vortical flow , 1997 .