A Comparative Study of Four Algebraic Transition Models

Paper #:
  • 941142

Published:
  • 1994-04-01
Citation:
Dorney, D., "A Comparative Study of Four Algebraic Transition Models," SAE Technical Paper 941142, 1994, https://doi.org/10.4271/941142.
Author(s):
Pages:
10
Abstract:
The flow through most turbomachinery blade rows is characterized by unsteady, viscous, transitional flow. The accurate prediction of the onset of transition from laminar to turbulent flow is essential for calculating heat transfer and performance quantities. The purpose of this investigation is to evaluate the accuracy of four different algebraic transition models which have been combined with an algebraic turbulence model. Numerical experiments have been performed for flow through a turbine rotor cascade with heat transfer, and a cascade of compressor blades. In addition, a study was performed to determine the effects of the computational grid density on the transition location.
Access
Now
SAE MOBILUS Subscriber? You may already have access.
Buy
Select
Price
List
Download
$27.00
Mail
$27.00
Members save up to 40% off list price.
Share
HTML for Linking to Page
Page URL

Related Items

Technical Paper / Journal Article
2011-04-12
Training / Education
2017-06-15
Standard
2002-10-21
Standard
2000-08-01
Standard
1994-03-01
Technical Paper / Journal Article
2011-04-12