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
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| Creator |
Romano, Diego Giuseppe
de Rosa, Donato Donelli, Raffaele Salvatore |
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| Subject |
Aerodynamics
Transition; Laminar flow; Turbulent flow CFD; Aerodynamics |
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| 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.
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| Publisher |
Associazione Italiana di Aeronautica e Astronautica (AIDAA)
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| Contributor |
—
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| Date |
2017-09-19
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| Type |
info:eu-repo/semantics/article
info:eu-repo/semantics/publishedVersion Peer-reviewed Article Numerical; Experimental comparison |
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| Format |
application/pdf
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| Identifier |
http://131.114.27.37/index.php/AMS/article/view/296
10.19249/ams.v96i1.296 |
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| Source |
Aerotecnica Missili & Spazio; Vol 96, No 1 (2017); 63-74
0365-7442 |
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| Language |
eng
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| Relation |
http://131.114.27.37/index.php/AMS/article/view/296/pdf
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| Rights |
Copyright (c) 2017 Aerotecnica Missili & Spazio
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