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Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft. / Roessler, Christian; Teubl, Daniel; Meddaikar, Yasser; Wüstenhagen, Matthias; Ossmann, Daniel; Sodja, Jurij; De Breuker, Roeland; Luspay, Tamás; Gyulai, László; More Authors.

AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL. AIAA, 2020. AIAA 2020-1969.

Research output: Chapter in Book/Conference proceedings/Edited volumeConference contributionScientificpeer-review

Harvard

Roessler, C, Teubl, D, Meddaikar, Y, Wüstenhagen, M, Ossmann, D, Sodja, J, De Breuker, R, Luspay, T, Gyulai, L & More Authors 2020, Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft. in AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL., AIAA 2020-1969, AIAA, AIAA Scitech 2020 Forum, Orlando, United States, 6/01/20. https://doi.org/10.2514/6.2020-1969

APA

Roessler, C., Teubl, D., Meddaikar, Y., Wüstenhagen, M., Ossmann, D., Sodja, J., ... More Authors (2020). Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft. In AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL [AIAA 2020-1969] AIAA. https://doi.org/10.2514/6.2020-1969

Vancouver

Roessler C, Teubl D, Meddaikar Y, Wüstenhagen M, Ossmann D, Sodja J et al. Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft. In AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL. AIAA. 2020. AIAA 2020-1969 https://doi.org/10.2514/6.2020-1969

Author

Roessler, Christian ; Teubl, Daniel ; Meddaikar, Yasser ; Wüstenhagen, Matthias ; Ossmann, Daniel ; Sodja, Jurij ; De Breuker, Roeland ; Luspay, Tamás ; Gyulai, László ; More Authors. / Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft. AIAA Scitech 2020 Forum: 6-10 January 2020, Orlando, FL. AIAA, 2020.

BibTeX

@inproceedings{3502ca40371f4640b1f754f6e02d072d,
title = "Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft",
abstract = "The idea of the EU funded FLEXOP project is to raise efficiency of a currently existing wing by derivative solution with higher aspect ratio at no excess structural weight. In order to enable such a resulting highly flexible wing the project goal is to develop methods for active suppression of flutter and passive load alleviation. The developed methods will be tested and validated with a UAV flutter demonstrator. The demonstrator is a 7m wingspan, 65kg MTOW UAV equipped with a jet engine. It features three different wing pairs. The first wing is a stiff design reference case, which is flown to get the baseline measurements for comparison. The second one is a wing designed very flexible specifically for active flutter control. The third wing is aeroelastically tailored for gust load alleviation. The paper describes the results of the aeroelastically tailored wing compared to the baseline reference wing.",
author = "Christian Roessler and Daniel Teubl and Yasser Meddaikar and Matthias W{\"u}stenhagen and Daniel Ossmann and Jurij Sodja and {De Breuker}, Roeland and Tam{\'a}s Luspay and L{\'a}szl{\'o} Gyulai and {More Authors}",
year = "2020",
doi = "10.2514/6.2020-1969",
language = "English",
booktitle = "AIAA Scitech 2020 Forum",
publisher = "AIAA",

}

RIS

TY - GEN

T1 - Results of an Aeroelastically Tailored Wing on the FLEXOP Demonstrator Aircraft

AU - Roessler, Christian

AU - Teubl, Daniel

AU - Meddaikar, Yasser

AU - Wüstenhagen, Matthias

AU - Ossmann, Daniel

AU - Sodja, Jurij

AU - De Breuker, Roeland

AU - Luspay, Tamás

AU - Gyulai, László

AU - More Authors, null

PY - 2020

Y1 - 2020

N2 - The idea of the EU funded FLEXOP project is to raise efficiency of a currently existing wing by derivative solution with higher aspect ratio at no excess structural weight. In order to enable such a resulting highly flexible wing the project goal is to develop methods for active suppression of flutter and passive load alleviation. The developed methods will be tested and validated with a UAV flutter demonstrator. The demonstrator is a 7m wingspan, 65kg MTOW UAV equipped with a jet engine. It features three different wing pairs. The first wing is a stiff design reference case, which is flown to get the baseline measurements for comparison. The second one is a wing designed very flexible specifically for active flutter control. The third wing is aeroelastically tailored for gust load alleviation. The paper describes the results of the aeroelastically tailored wing compared to the baseline reference wing.

AB - The idea of the EU funded FLEXOP project is to raise efficiency of a currently existing wing by derivative solution with higher aspect ratio at no excess structural weight. In order to enable such a resulting highly flexible wing the project goal is to develop methods for active suppression of flutter and passive load alleviation. The developed methods will be tested and validated with a UAV flutter demonstrator. The demonstrator is a 7m wingspan, 65kg MTOW UAV equipped with a jet engine. It features three different wing pairs. The first wing is a stiff design reference case, which is flown to get the baseline measurements for comparison. The second one is a wing designed very flexible specifically for active flutter control. The third wing is aeroelastically tailored for gust load alleviation. The paper describes the results of the aeroelastically tailored wing compared to the baseline reference wing.

U2 - 10.2514/6.2020-1969

DO - 10.2514/6.2020-1969

M3 - Conference contribution

BT - AIAA Scitech 2020 Forum

PB - AIAA

ER -

ID: 68467514