Correction: Aerodynamic Benefits of Camber Morphing Technology for Strut-Braced Wing Configurations (American Institute of Aeronautics and Astronautics Inc, AIAA)

Ilias Tsatsas; Emanuele Sticchi; Xavier Carrillo Córcoles; Roeland De Breuker; Jurij Sodja

doi:10.2514/6.2025-0281.c1

Correction: Aerodynamic Benefits of Camber Morphing Technology for Strut-Braced Wing Configurations (American Institute of Aeronautics and Astronautics Inc, AIAA)

Ilias Tsatsas, Emanuele Sticchi, Xavier Carrillo Córcoles, Roeland De Breuker, Jurij Sodja

Research output: Contribution to journal › Comment/Letter to the editor › Scientific › peer-review

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Abstract

Correction notice The CL in the title of Fig. 7(b) was corrected from 0.4 in the original version to CL=1.0. (a) Climb local lift spanwise distribution at CL=1 0 0.2 0.4 0.6 0.8 1 0 5 10 10-3 0 0.2 0.4 0.6 0.8 1 0 5 10 10-3 (b) Solid line (suction side)-dashed line (pressure side) Fig. 7 Local lift coefficient distribution with a selected friction coefficient of one section.

Original language	English
Number of pages	1
Journal	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
DOIs	https://doi.org/10.2514/6.2025-0281.c1
Publication status	Published - 2025
Event	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 - Orlando, United States Duration: 6 Jan 2025 → 10 Jan 2025

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10.2514/6.2025-0281.c1

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@article{062a7c391b0046b8a8e5e6e7f422687c,

title = "Correction: Aerodynamic Benefits of Camber Morphing Technology for Strut-Braced Wing Configurations (American Institute of Aeronautics and Astronautics Inc, AIAA)",

abstract = " Correction notice The CL in the title of Fig. 7(b) was corrected from 0.4 in the original version to CL=1.0. (a) Climb local lift spanwise distribution at CL=1 0 0.2 0.4 0.6 0.8 1 0 5 10 10-3 0 0.2 0.4 0.6 0.8 1 0 5 10 10-3 (b) Solid line (suction side)-dashed line (pressure side) Fig. 7 Local lift coefficient distribution with a selected friction coefficient of one section.",

author = "Ilias Tsatsas and Emanuele Sticchi and C{\'o}rcoles, {Xavier Carrillo} and {De Breuker}, Roeland and Jurij Sodja",

year = "2025",

doi = "10.2514/6.2025-0281.c1",

language = "English",

journal = "AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025",

note = "AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 ; Conference date: 06-01-2025 Through 10-01-2025",

}

Correction: Aerodynamic Benefits of Camber Morphing Technology for Strut-Braced Wing Configurations (American Institute of Aeronautics and Astronautics Inc, AIAA). / Tsatsas, Ilias ; Sticchi, Emanuele ; Córcoles, Xavier Carrillo et al.
In: AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025, 2025.

Research output: Contribution to journal › Comment/Letter to the editor › Scientific › peer-review

TY - JOUR

T1 - Correction

T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025

AU - Tsatsas, Ilias

AU - Sticchi, Emanuele

AU - Córcoles, Xavier Carrillo

AU - De Breuker, Roeland

AU - Sodja, Jurij

PY - 2025

Y1 - 2025

N2 - Correction notice The CL in the title of Fig. 7(b) was corrected from 0.4 in the original version to CL=1.0. (a) Climb local lift spanwise distribution at CL=1 0 0.2 0.4 0.6 0.8 1 0 5 10 10-3 0 0.2 0.4 0.6 0.8 1 0 5 10 10-3 (b) Solid line (suction side)-dashed line (pressure side) Fig. 7 Local lift coefficient distribution with a selected friction coefficient of one section.

AB - Correction notice The CL in the title of Fig. 7(b) was corrected from 0.4 in the original version to CL=1.0. (a) Climb local lift spanwise distribution at CL=1 0 0.2 0.4 0.6 0.8 1 0 5 10 10-3 0 0.2 0.4 0.6 0.8 1 0 5 10 10-3 (b) Solid line (suction side)-dashed line (pressure side) Fig. 7 Local lift coefficient distribution with a selected friction coefficient of one section.

UR - http://www.scopus.com/inward/record.url?scp=105001471969&partnerID=8YFLogxK

U2 - 10.2514/6.2025-0281.c1

DO - 10.2514/6.2025-0281.c1

M3 - Comment/Letter to the editor

AN - SCOPUS:105001471969

JO - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025

JF - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025

Y2 - 6 January 2025 through 10 January 2025

ER -

Correction: Aerodynamic Benefits of Camber Morphing Technology for Strut-Braced Wing Configurations (American Institute of Aeronautics and Astronautics Inc, AIAA)

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