Optimization, manufacturing and testing of a composite wing with maximized tip deflection

YM Meddaikar; JKS Dillinger; J Sodja; H Mai; R de Breuker

doi:10.2514/6.2016-0489

Optimization, manufacturing and testing of a composite wing with maximized tip deflection

YM Meddaikar, JKS Dillinger, J Sodja, H Mai, R de Breuker

Aerospace Structures & Computational Mechanics

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

Original language	English
Title of host publication	Proceedings of the 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference
Editors	s.n.
Place of Publication	Reston
Publisher	American Institute of Aeronautics and Astronautics Inc. (AIAA)
Pages	1-11
Number of pages	11
ISBN (Print)	978-1-62410-392-6
DOIs	https://doi.org/10.2514/6.2016-0489
Publication status	Published - 2016
Event	57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference - San Diego, United States Duration: 4 Jan 2016 → 8 Jan 2016 Conference number: 57

Publication series

Name
Publisher	AIAA

Conference

Conference	57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference
Country	United States
City	San Diego
Period	4/01/16 → 8/01/16

Access to Document

10.2514/6.2016-0489

Cite this

Meddaikar, YM., Dillinger, JKS., Sodja, J., Mai, H., & de Breuker, R. (2016). Optimization, manufacturing and testing of a composite wing with maximized tip deflection. In s.n. (Ed.), Proceedings of the 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference (pp. 1-11). American Institute of Aeronautics and Astronautics Inc. (AIAA). https://doi.org/10.2514/6.2016-0489

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Meddaikar, YM, Dillinger, JKS , Sodja, J, Mai, H & de Breuker, R 2016, Optimization, manufacturing and testing of a composite wing with maximized tip deflection. in s.n. (ed.), Proceedings of the 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference. American Institute of Aeronautics and Astronautics Inc. (AIAA), Reston, pp. 1-11, 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference, San Diego, United States, 4/01/16. https://doi.org/10.2514/6.2016-0489

Optimization, manufacturing and testing of a composite wing with maximized tip deflection. / Meddaikar, YM; Dillinger, JKS ; Sodja, J; Mai, H; de Breuker, R.

Proceedings of the 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference. ed. / s.n. Reston : American Institute of Aeronautics and Astronautics Inc. (AIAA), 2016. p. 1-11.

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

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AU - Mai, H

AU - de Breuker, R

N1 - Conference code: 57

PY - 2016

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M3 - Conference contribution

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BT - Proceedings of the 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference

A2 - s.n., null

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

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T2 - 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference

Y2 - 4 January 2016 through 8 January 2016

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Meddaikar YM, Dillinger JKS , Sodja J, Mai H, de Breuker R. Optimization, manufacturing and testing of a composite wing with maximized tip deflection. In s.n., editor, Proceedings of the 57th AIAA/ASCE/AHS/ASC structures, structural dynamics, and materials conference. Reston: American Institute of Aeronautics and Astronautics Inc. (AIAA). 2016. p. 1-11 https://doi.org/10.2514/6.2016-0489