Challenges, ideas, and innovations of joined-wing configurations: a concept from the past, an opportunity for the future

R Cavallaro, L Demasi - Progress in Aerospace Sciences, 2016 - Elsevier
Abstract Diamond Wings, Strut-and Truss-Braced Wings, Box Wings, and PrandtlPlane, the
so-called “JoinedWings”, represent a dramatic departure from traditional configurations …

[HTML][HTML] The enabling technologies for a quasi-zero emissions commuter aircraft

D Ciliberti, P Della Vecchia, V Memmolo, F Nicolosi… - Aerospace, 2022 - mdpi.com
The desire for greener aircraft pushes both academic and industrial research into
develo** technologies, manufacturing, and operational strategies providing emissions …

Collaborative Pazy wing analyses for the third aeroelastic prediction workshop

M Ritter, J Hilger, A Ribeiro, AE Öngüt, M Righi… - AIAA SciTech 2024 …, 2024 - arc.aiaa.org
In this paper, collaborative aeroelastic analyses of the\textit {Pazy Wing} are presented,
which support the activities of the Large Deflection Working Group, a sub-group of the 3rd …

[HTML][HTML] Flutter and gust response analysis of a wing model including geometric nonlinearities based on a modified structural ROM

AN Chao, Y Chao, X Changchuan, Y Lan - Chinese Journal of Aeronautics, 2020 - Elsevier
In this paper, a framework is established for nonlinear flutter and gust response analyses
based on an efficient Reduced Order Model (ROM). The proposed method can be used to …

Rapid transonic flutter analysis for aircraft conceptual design applications

W Mallik, JA Schetz, RK Kapania - AIAA Journal, 2018 - arc.aiaa.org
This study presents a new approach for the rapid transonic flutter analysis of large-aspect-
ratio wings via a combination of time-linearized two-dimensional unsteady indicial functions …

A refined aeroelastic beam finite element for the stability analysis of flexible subsonic wings

CR Vindigni, G Mantegna, C Orlando, A Alaimo… - Computers & …, 2025 - Elsevier
In this work, a novel finite element approach for the computational aeroelastic analysis of
flexible lifting structures in subsonic flow is presented. The numerical simulation of the fluid …

Parametric Aeroservoelastic-Gust Reduced-Order Models with State Consistence Enforcement

J Kim, JI Shu, Y Wang, J Simac… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
This paper presents a novel data-driven, parametric AeroServoElastic-Gust reduced-order
models (ASEG-ROMs) in the state-space form to capture complex dynamic interactions …

Structural and aeroelastic design, analysis, and experiments of inflatable airborne wings

W Zhao, S Desai, J Miglani, RK Kapania… - AIAA SciTech 2021 …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1817. vid A scaled, tethered
inflatable wing wind tunnel model is studied to investigate its aeroelastic response as a …

Configurable Parametric Aeroservoelastic-Gust Reduced-Order Models with State-Consistence Enforcement

J Kim, JI Shu, Y Wang, J Simac, A Kaminsky - AIAA Journal, 2024 - arc.aiaa.org
Parametric reduced-order models (ROMs) across various flight regimes are crucial for rapid
aeroelastic and gust load analysis and aerostructure control synthesis. This paper presents …

Analysis, design, and experiments of metal flat plate and foam airfoil flutter test articles

J Miglani, W Zhao, S Desai, V Sanmugadas… - AIAA Scitech 2021 …, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1497. vid The Virginia Tech 0.7 m *
0.7 m Open Jet Wind Tunnel was used to test two different flutter test articles to understand …