Navier–Stokes Solution for Steady Two-Dimensional Transonic Cascade Flows

[+] Author and Article Information
O. K. Kwon

Allison Gas Turbine Division, General Motors Corporation, Indianapolis, IN

J. Turbomach 110(3), 339-346 (Jul 01, 1988) (8 pages) doi:10.1115/1.3262202 History: Received February 04, 1987; Online November 09, 2009


A robust, time-marching Navier–Stokes solution procedure based on the explicit hopscotch method is presented for solution of steady, two-dimensional, transonic turbine cascade flows. The method is applied to the strong conservation form of the unsteady Navier–Stokes equations written in arbitrary curvilinear coordinates. Cascade flow solutions are obtained on an orthogonal, body-conforming “O” grid with the standard k –ε turbulence model. Computed results are presented and compared with experimental data.

Copyright © 1988 by ASME
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In