A Three-Dimensional Structured/unstructured Hybrid Navier-Stokes Method for Turbine Blade Rows
Author(s) -
Fu-Lin Tsung,
J. Loellbach,
Ohjoon Kwon,
Chunill Hah
Publication year - 1994
Publication title -
28th joint propulsion conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1994-3369
Subject(s) - blade (archaeology) , row , turbine blade , computer science , row and column spaces , turbine , mechanical engineering , engineering , database
A three-dimensional viscous structured/unstructured hybrid scheme has been developed for numerical computation of high Reynolds number turbomachinery flows. The procedure allows an efficient structured solver to be employed in the densely clustered, high aspect-ratio grid around the viscous regions near solid surfaces, while employing an unstructured solver elsewhere in the flow domain to add flexibility in mesh generation. Test results for an inviscid flow over an external transonic wing and a Navier-Stokes flow for an internal annular cascade are presented.
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom