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

Journal article (2025)

Authors

I. Tsatsas Group De Breuker, Arts & Crafts
Emanuele Sticchi Wind Energy
R. De Breuker Aerospace Structures & Materials
Jurij Sodja Group Sodja
Research Group
Group De Breuker
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Published Date

2025

Language

English

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Research Group

Group De Breuker

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.

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