Design of a swept wing wind tunnel model for study of cross-flow instability

J Serpieri; M Kotsonis

doi:10.2514/6.2015-2576

Design of a swept wing wind tunnel model for study of cross-flow instability

Aerodynamics

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

13 Citations (Scopus)

Original language	English
Title of host publication	Proceedings of the 33rd AIAA applied aerodynamics conference
Editors	s.n.
Place of Publication	Reston
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages	1-15
Number of pages	15
ISBN (Print)	978-1-62410-363-6
DOIs	https://doi.org/10.2514/6.2015-2576
Publication status	Published - 2015
Event	33rd AIAA applied aerodynamics conference, Dallas, USA - Reston Duration: 22 Jun 2015 → 26 Jun 2015

Publication series

Name
Publisher	AIAA

Conference

Conference	33rd AIAA applied aerodynamics conference, Dallas, USA
Period	22/06/15 → 26/06/15

Bibliographical note

harvest
AIAA 2015-2576

Access to Document

10.2514/6.2015-2576

Cite this

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title = "Design of a swept wing wind tunnel model for study of cross-flow instability",

author = "J Serpieri and M Kotsonis",

note = "harvest AIAA 2015-2576; 33rd AIAA applied aerodynamics conference, Dallas, USA ; Conference date: 22-06-2015 Through 26-06-2015",

year = "2015",

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language = "English",

isbn = "978-1-62410-363-6",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

pages = "1--15",

editor = "s.n.",

booktitle = "Proceedings of the 33rd AIAA applied aerodynamics conference",

address = "United States",

}

Serpieri, J & Kotsonis, M 2015, Design of a swept wing wind tunnel model for study of cross-flow instability. in s.n. (ed.), Proceedings of the 33rd AIAA applied aerodynamics conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), Reston, pp. 1-15, 33rd AIAA applied aerodynamics conference, Dallas, USA, 22/06/15. https://doi.org/10.2514/6.2015-2576

Design of a swept wing wind tunnel model for study of cross-flow instability. / Serpieri, J; Kotsonis, M.
Proceedings of the 33rd AIAA applied aerodynamics conference. ed. / s.n. Reston: American Institute of Aeronautics and Astronautics Inc. (AIAA), 2015. p. 1-15.

Research output: Chapter in Book/Conference proceedings/Edited volume › Conference contribution › Scientific › peer-review

TY - GEN

T1 - Design of a swept wing wind tunnel model for study of cross-flow instability

AU - Serpieri, J

AU - Kotsonis, M

N1 - harvest AIAA 2015-2576

PY - 2015

Y1 - 2015

U2 - 10.2514/6.2015-2576

DO - 10.2514/6.2015-2576

M3 - Conference contribution

SN - 978-1-62410-363-6

SP - 1

EP - 15

BT - Proceedings of the 33rd AIAA applied aerodynamics conference

A2 - s.n., null

PB - American Institute of Aeronautics and Astronautics Inc. (AIAA)

CY - Reston

T2 - 33rd AIAA applied aerodynamics conference, Dallas, USA

Y2 - 22 June 2015 through 26 June 2015

ER -