Morphing Winglet Design for Aerodynamic Performance Optimization of the CRJ-700 Aircraft. Part 1 – Structural Design
نویسندگان
چکیده
This study aims to design a morphing winglet structure for the CRJ-700 regional transport aircraft. The technology is applied on winglets demonstrate significant increase of aerodynamic performance From data LARCASE Virtual Research Simulator VRESIM, benefits in cruising phase were obtained through ParaView software. was drawn using CATIA V5; this new concept included several structural components, as well simple and light mechanism allowing orientate angles between 90° -90° inclination. model exported HyperMesh analysis Maximum stresses obtained, demonstrated its resistance maximum loads load factors -2G 7G.
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ژورنال
عنوان ژورنال: INCAS Buletin
سال: 2021
ISSN: ['2066-8201', '2247-4528']
DOI: https://doi.org/10.13111/2066-8201.2021.13.4.10