The use of RANS approach for predicting transition

Aerotecnica Missili & Spazio

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Field Value
 
Title The use of RANS approach for predicting transition
 
Creator Russo, Serena
 
Subject Aerodynamics; Flight Mechanics;
Transition prediction, RANS, turbulence

 
Description A numerical procedure to improve the performances of a Reynolds--Averaged Navier--Stokes code by including an accurate prediction of the location of the transition onset is presented. A transition prediction module is coupled with the Ansys Fluent flow solver. The transition prediction is obtained with a CIRA--ONERA data--base method based on the analytical representation of the growth rate for the disturbances as a function of some relevant boundary layer parameters. A preliminary 2D test case will be considered and, then, a real model of wing.
 
Publisher Associazione Italiana di Aeronautica e Astronautica (AIDAA)
 
Contributor
 
Date 2018-10-22
 
Type info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
Peer-reviewed Article
Numerical
 
Format application/pdf
 
Identifier http://131.114.27.37/index.php/AMS/article/view/321
10.19249/ams.v97i3.321
 
Source Aerotecnica Missili & Spazio; Vol 97, No 3 (2018); 145-152
0365-7442
 
Language eng
 
Relation http://131.114.27.37/index.php/AMS/article/view/321/pdf
 
Rights Copyright (c) 2018 Aerotecnica Missili & Spazio
 

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