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On the Aeroelasticity of a Cantilever Wing Equipped with the Spanwise Morphing Trailing Edge Concept (2023)
Journal Article
Pilakkadan, J. S., Ajaj, R. M., Haider, Z., & Amoozgar, M. (2023). On the Aeroelasticity of a Cantilever Wing Equipped with the Spanwise Morphing Trailing Edge Concept. Aerospace, 10(9), Article 809. https://doi.org/10.3390/aerospace10090809

This paper studies the aeroelastic behavior of a rectangular, cantilever wing equipped with the spanwise morphing trailing edge (SMTE) concept. The SMTE consists of multiple trailing edge flaps that allow controlling the spanwise camber distribution... Read More about On the Aeroelasticity of a Cantilever Wing Equipped with the Spanwise Morphing Trailing Edge Concept.

Vibration Attenuation of Rotating Blades Using a Non-Linear Energy Sink (2023)
Conference Proceeding
Wall, I. P., Amoozgar, M., & Popov, A. (2023). Vibration Attenuation of Rotating Blades Using a Non-Linear Energy Sink. In AIAA 2023-3952 Session: Applied Aeroelasticity and Aerodynamic-Structural Dynamics Interaction II. https://doi.org/10.2514/6.2023-3952

The global climate crisis is placing higher demands on the performance of wind turbines. One of the promising methods to enhance the wind turbine performance is to increase the rotor diameter by having larger blades. However, the blade length is alwa... Read More about Vibration Attenuation of Rotating Blades Using a Non-Linear Energy Sink.

Engine Placement Effects on the Flutter of a Medium-Range Box-Wing Aircraft (2023)
Journal Article
Ghasemikaram, A. H., Mazidi, A., Fazelzadeh, S. A., & Amoozgar, M. (2023). Engine Placement Effects on the Flutter of a Medium-Range Box-Wing Aircraft. Journal of Aerospace Engineering, 36(4), https://doi.org/10.1061/JAEEEZ.ASENG-4753

This study investigated the effects of powered engines on the stability boundaries of a box-wing configuration. The governing equations were obtained using Hamilton's principle. The equivalent effects of engine's mass and thrust were simulated using... Read More about Engine Placement Effects on the Flutter of a Medium-Range Box-Wing Aircraft.