Zobrazeno 1 - 10
of 72
pro vyhledávání: '"James J. Joo"'
Publikováno v:
Mechanics Based Design of Structures and Machines. :1-23
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2023 Forum.
Autor:
Christina Harvey, Lawren L. Gamble, Christian R. Bolander, Douglas F. Hunsaker, James J. Joo, Daniel J. Inman
Publikováno v:
Mechanical and Aerospace Engineering Faculty Publications
The impressive maneuverability demonstrated by birds has so far eluded comparably sized uncrewed aerial vehicles (UAVs). Modern studies have shown that birds’ ability to change the shape of their wings and tail in flight, known as morphing, allows
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e0fd76284ddb25cee59c51599a9ca2b4
https://digitalcommons.usu.edu/context/mae_facpub/article/1206/viewcontent/MAEfacpub2022HarveyGambleBolander_ReviewAvianInspired.pdf
https://digitalcommons.usu.edu/context/mae_facpub/article/1206/viewcontent/MAEfacpub2022HarveyGambleBolander_ReviewAvianInspired.pdf
Publikováno v:
Journal of Mechanisms and Robotics. 14
This paper presents a mechanism design optimization for actuating the horizontal stabilizers of an aircraft using a rotating empennage without a vertical stabilizer. Birds do not have vertical stabilizers and rotate their tail feathers to control agi
Publikováno v:
AIAA Journal. 58:2909-2920
Lifting-line theory has formed the basis of wing-design understanding for nearly a century. This theory has previously been used to develop a class of optimal lift distributions that minimize induc...
Publikováno v:
Volume 8A: 45th Mechanisms and Robotics Conference (MR).
This paper presents a mechanism design optimization for actuating the horizontal stabilizers of an aircraft using a rotating empennage without a vertical stabilizer. Birds do not have vertical stabilizers and rotate their tail feathers to control agi
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:788-803
Geometric and/or aerodynamic wing twist can be used to produce a lift distribution that results in a rolling moment. A decomposed Fourier-series solution to Prandtl’s lifting-line theory is used to develop analytic spanwise antisymmetric twist dist
Publikováno v:
Journal of Aircraft. 56:431-441
Minimum induced drag for fixed gross weight and wingspan is obtained from the elliptic lift distribution. However, minimum induced drag for steady level flight is not obtained by imposing the const...
Publikováno v:
ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik. 101