Numerical and Experimental Transition Prediction on a Realistic Laminar Swept Wing

Aerotecnica Missili & Spazio

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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)
Date 2017-09-19
Type info:eu-repo/semantics/article
Peer-reviewed Article
Numerical; Experimental comparison
Format application/pdf
Source Aerotecnica Missili & Spazio; Vol 96, No 1 (2017); 63-74
Language eng
Rights Copyright (c) 2017 Aerotecnica Missili & Spazio

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