Unsteady Aeroelastic Analysis of the Semi Aeroelastic Hinge Including Local Geometric Nonlinearities

Autor: Paolo Mastracci, Francesco Saltari, Franco Mastroddi, Thomas Wilson, Andrea Castrichini

Publikováno v: AIAA Journal. 60:3147-3165

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::03df1ec7a1bc418688dd99b5e73007c0
https://doi.org/10.2514/1.j061108

Experimental and numerical investigation of an aircraft wing with hinged wingtip for gust load alleviation

Autor: Davide Balatti, Hamed Haddad Khodaparast, Michael I. Friswell, Marinos Manolesos, Andrea Castrichini

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1cab5c73a03d4d55888973fecca23202
https://cronfa.swan.ac.uk/Record/cronfa63238

Aeroelastics Flight Dynamics Coupling Effects of the Semi-Aeroelastic Hinge Device

Autor: Jonathan E. Cooper, Thomas Wilson, Andrea Castrichini, Franco Mastroddi, N. Viceconti, Francesco Saltari

Publikováno v: Castrichini, A, Wilson, T, Salteri, F, Mastroddi,, F, Viceconti, N & Cooper, J E 2019, ' Aeroelastics Flight Dynamics Coupling Effects of the Semi Aeroelastic Hinge Device ', Journal of Aircraft . https://doi.org/10.2514/1.C035602

A recent consideration in aircraft design is the use of folding wing-tips with the aim of enabling higher aspect ratio aircraft with less induced drag, but also meeting airport gate limitations. This study investigates the impact of floating folding

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c1596811fa350645038caa6a87a93306
https://doi.org/10.2514/1.c035602

Experimental Analysis of the Dynamics of Flared Folding Wingtips via a Novel Tethered Flight Test

Autor: Fintan Healy, Alessandro Pontillo, Djamel Rezgui, Jonathan E. Cooper, James Kirk, Thomas Wilson, Andrea Castrichini

Publikováno v: Healy, F, Pontillo, A, Rezgui, D, Cooper, J E, Kirk, J, Wilson, T & Castrichini, A 2021, Experimental Analysis of the Dynamics of Flared Folding Wingtips via a Novel Tethered Flight Test . in AIAA SCITECH 2022 Forum : Session: Flexible Aeroelastic Problems of Unmanned Air Vehicles of All Scales . American Institute of Aeronautics and Astronautics Inc. (AIAA), 2022 AIAA SciTech Forum, San Diego, United States, 3/01/22 . https://doi.org/10.2514/6.2022-1757

Recent developments in morphing wing technologies are routinely tested using Unmanned Aerial vehicles (UAVs) due to their relatively low cost and time to manufacture. However, atmospheric flight tests limit both the repeatability of the recorded data

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f2ea4e99e77a3cd8fdc22ea5237236a0
https://hdl.handle.net/1983/0d1bfa37-458c-4689-ac78-df6a5cd606d4

Folding Wingtips for Improved Roll Performance

Autor: Ronald C M Cheung, Djamel Rezgui, Andrea Castrichini, Thomas Wilson, Mark H Lowenberg, Fintan Healy, Theodore Neofet, Jonathan E. Cooper

Publikováno v: Healy, F, Cheung, R C M, Neofet, T, Lowenberg, M H, Rezgui, D, Cooper, J E, Castrichini, A & Wilson, T 2021, ' Folding Wingtips for Improved Roll Performance ', Journal of Aircraft . https://doi.org/10.2514/1.C036372
Healy, F, Cheung, R C M, Neofet, T, Lowenberg, M H, Rezgui, D, Cooper, J E, Castrichini, A & Wilson, T 2021, Folding Wingtips for Improved Roll Performance . in AIAA Scitech 2021 Forum . AIAA Scitech 2021 Forum, American Institute of Aeronautics and Astronautics Inc. (AIAA), pp. 1-24, 2021 AIAA SciTech Forum, 4/01/21 . https://doi.org/10.2514/6.2021-1153

Future aircraft designs look set to use longer wing spans to increase the aspect ratio and therefore overall aerodynamic efficiency of the airframe. Such larger wing spans also reduce roll rates and require increased control surface area to achieve t

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cf8d40484a682ea1f2722e3faf553e0d
https://research-information.bris.ac.uk/en/publications/6b6a1ddb-307b-4c81-bce7-d542cbb7bc09