Numerical and Experimental Transition Prediction on a Realistic Laminar Swept Wing

Aerotecnica Missili & Spazio

View Publication Info
 
 
Field Value
 
Title Numerical and Experimental Transition Prediction on a Realistic Laminar Swept Wing
 
Creator Romano, Diego Giuseppe
de Rosa, Donato
Donelli, Raffaele Salvatore
 
Subject Aerodynamics
Transition; Laminar flow; Turbulent flow
CFD; Aerodynamics
 
Description This paper is aimed at providing the outcomes of an activity carried out inside an Italian National Program named VITAS (Vettore Innovativo per il Trasporto AeroSostenibile).The goal of the project was to design a transonic wing with an extended natural laminar region for a business jet (8-12 seats).Both experimental and numerical activities were carried out in order to define and verify the performance of this laminar wing. The paper will deal with the numerical activities, experimental/numerical comparison will be shown and results will be discussed.
 
Publisher Associazione Italiana di Aeronautica e Astronautica (AIDAA)
 
Contributor
 
Date 2017-09-19
 
Type info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion
Peer-reviewed Article
Numerical; Experimental comparison
 
Format application/pdf
 
Identifier http://131.114.27.37/index.php/AMS/article/view/296
10.19249/ams.v96i1.296
 
Source Aerotecnica Missili & Spazio; Vol 96, No 1 (2017); 63-74
0365-7442
 
Language eng
 
Relation http://131.114.27.37/index.php/AMS/article/view/296/pdf
 
Rights Copyright (c) 2017 Aerotecnica Missili & Spazio
 

Contact Us

The PKP Index is an initiative of the Public Knowledge Project.

For PKP Publishing Services please use the PKP|PS contact form.

For support with PKP software we encourage users to consult our wiki for documentation and search our support forums.

For any other correspondence feel free to contact us using the PKP contact form.

Find Us

Twitter

Copyright © 2015-2018 Simon Fraser University Library