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Challenges, ideas, and innovations of joined-wing configurations: a concept from the past, an opportunity for the future
Abstract Diamond Wings, Strut-and Truss-Braced Wings, Box Wings, and PrandtlPlane, the
so-called “JoinedWings”, represent a dramatic departure from traditional configurations …
so-called “JoinedWings”, represent a dramatic departure from traditional configurations …
[HTML][HTML] The enabling technologies for a quasi-zero emissions commuter aircraft
The desire for greener aircraft pushes both academic and industrial research into
develo** technologies, manufacturing, and operational strategies providing emissions …
develo** technologies, manufacturing, and operational strategies providing emissions …
Collaborative Pazy wing analyses for the third aeroelastic prediction workshop
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 …
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 …
based on an efficient Reduced Order Model (ROM). The proposed method can be used to …
Rapid transonic flutter analysis for aircraft conceptual design applications
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 …
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
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 …
flexible lifting structures in subsonic flow is presented. The numerical simulation of the fluid …
Parametric Aeroservoelastic-Gust Reduced-Order Models with State Consistence Enforcement
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 …
models (ASEG-ROMs) in the state-space form to capture complex dynamic interactions …
Structural and aeroelastic design, analysis, and experiments of inflatable airborne wings
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 …
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
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 …
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
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 …
0.7 m Open Jet Wind Tunnel was used to test two different flutter test articles to understand …