Theoretic analysis and experiment on aeroelasticity of very flexible wing
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- Type
- article
- Published
- 2012-07-11
- Cited by
- 14
- References
- 8
- OpenAlex
- https://openalex.org/W2075246250
- Semantic Scholar
- https://api.semanticscholar.org/CorpusID:122499561
Keywords
Aeroelasticity, Wing, Wing configuration, Structural engineering, Aerospace engineering
References
- Nonlinear aeroelastic analysis, flight dynamics, and control of a complete aircraft
- On the importance of aerodynamic and structural geometrical nonlinearities in aeroelastic behavior of high-aspect-ratio wings $
- Modern Adaptation of Prandtl's Classic Lifting-Line Theory
- Experimental and Theoretical Study on Aeroelastic Response of High-Aspect-Ratio Wings
- Geometrical nonlinear aeroelastic stability analysis of a composite high-aspect-ratio wing
- Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft
- Linearization method of nonlinear aeroelastic stability for complete aircraft with high-aspect-ratio wings
- Flutter Analysis of Wing Configurations Using Pre-Stressed Frequencies and Mode Shapes
- Influence of chordwise bending stiffness on aeroelastic characteristics of flexible high-aspect-ratio wing
- Nonlinear Aeroelasticity
Cited by
- Design and aerodynamic investigation of a parallel vehicle on a wide-speed range
- Gust response analysis and wind tunnel test for a high-aspect ratio wing
- Dynamic Response of Aeroelastically Tailored Composite Wing: Analysis and Experiment
- A review on non-linear aeroelasticity of high aspect-ratio wings
- Flutter analysis of a morphing wing technology demonstrator: Numerical simulation and wind tunnel testing
- Aeroelastic Optimization Design for High-Aspect-Ratio Wings with Large Deformation
- A comparative study of nonlinear aeroelastic models for high aspect ratio wings
- Aeroelastic Modeling and Analysis of High Aspect Ratio Wings With Different Fidelity Structural Models
- Flexible Unmanned Arial Vehicles and the Study of Their Special Aeroelasticity
- Time-domain nonlinear aeroelastic analysis and wind tunnel test of a flexible wing using strain-based beam formulation
- Estimation of the divergence characteristics of a jet transport aircraft wing using numerical method.
- Experimental investigations on structural improvement of morphing mechanism for nose cone of aerospace vehicle adopting a bionic redundant constraint strategy
- Aeroelastic Analysis of Aircraft Wings
- Nonlinear Flutter Test of a Very Flexible Wing
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