Title
Aerodynamic Aspects And Cooling Techniques Of Turbine Blade; Numerical Studies Using Urans And Les
Abstract
Numerical investigations of turbine blade are carried out using unsteady Reynolds-averaged Navier-Stokes (URANS) and large eddy simulation (LES) techniques. The goal of the present studies is to investigate the turbine blade aerodynamics and blade cooling techniques. The simulations are performed for a Reynolds number, Re = 1.3 x 106, based on the chord, c, of the airfoil and free-stream velocity. The computational results reveal the dissipative nature, of URANS, associated with the turbulence modeling. © 2011 by Marcel Ilie.
Publication Date
1-1-2011
Publication Title
29th AIAA Applied Aerodynamics Conference 2011
Number of Pages
-
Document Type
Article; Proceedings Paper
Personal Identifier
scopus
DOI Link
https://doi.org/10.2514/6.2011-3360
Copyright Status
Unknown
Socpus ID
85067319229 (Scopus)
Source API URL
https://api.elsevier.com/content/abstract/scopus_id/85067319229
STARS Citation
Al-Kuran, Husam; Velez, Carlos; Coronado, Patricia; and Ilie, Marcel, "Aerodynamic Aspects And Cooling Techniques Of Turbine Blade; Numerical Studies Using Urans And Les" (2011). Scopus Export 2010-2014. 3108.
https://stars.library.ucf.edu/scopus2010/3108