Aeroelastic Stability Analysis of Electric Aircraft Wings with Distributed Electric Propulsors
Aerospace, 2021 In this paper, the effect of distributed electric propulsion on the aeroelastic stability of an electric aircraft wing was investigated. All the electric propulsors, which are of different properties, are attached to the wing of the aircraft in different
Mohammadreza Amoozgar +5 more
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Helicopter Blade Stability Analysis Using Aeroelastic Frequency Response Functions
Journal of Applied and Computational Mechanics, 2015 In the present paper, the aeroelastic stability of helicopter rotor blade is determined using Aeroelastic Frequency Response Function. The aeroelastic model of blade is obtained by combining Dowell - Hodges beam model with Loewy unsteady aerodynamic ...
Mostafa Mohagheghi +2 more
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A Modal Interpretation for Aeroelastic Stability Enhancement of Mistuned Bladed Disks
Aerospace, 2022 Understanding the mechanism of the aeroelastic stability improvement induced by mistuning is essential for the design of bladed disks in aero-engines. In this paper, a quantitative interpretation is given. It starts by projecting the mistuned aeroelastic
Xin Liu, Yu Fan, Lin Li, Xiaoping Yu
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Aeroelastic stability analysis using linear matrix inequalities [PDF]
Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2012 The present work describes an alternative methodology for identification of aeroelastic stability in a range of varying parameters. Analysis is performed in time domain based on Lyapunov stability and solved by convex optimization algorithms. The theory is outlined and simulations are carried out on a benchmark system to illustrate the method.
Bueno, Douglas D. +3 more
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Influence of structure parameters on aeroelastic stability for labyrinth seal based on energy method
Propulsion and Power Research, 2018 Numerical analysis of turbomachinery based on energy method is used to predict the aeroelastic stability of the straight-through labyrinth seal by solving aerodynamic work and damping.
Nengmao Wang, Yanrong Wang, Aimei Tian
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Investigation of Stall Flutter Based on Peters-ONERA Aerodynamic Model [PDF]
Xibei Gongye Daxue Xuebao, 2018 The Peters model is used to simulate the linear aerodynamic force and ONERA stall model is used to simulate the nonlinear aerodynamic force. The state-space equation of the aeroelastic system is established by coupling the structural equation.
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Aeroelastic Response of Spinning Projectiles with Large Slenderness Ratio at Supersonic Speed
Aerospace, 2023 Obvious aeroelastic deformation occurs in spinning projectiles with large slenderness ratio, which seriously affects flight stability and maneuverability.
Qi Liu +3 more
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A numerical investigation into the aerodynamic characteristics and aeroelastic stability of a footbridge [PDF]
, 2009 The results of a numerical investigation into the aerodynamic characteristics and aeroelastic stability of a proposed footbridge across a highway in the north of England are presented.
Taylor, I.J., Vezza, M.
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Maneuverable unmanned aerial vehicle "rudder - drive” system design for aeroelastic stability
Научный вестник МГТУ ГА, 2019 The article considers the technique of designing a "rudder - drive" system aimed at ensuring safety from flutter of the flight control that is the aerodynamic rudder and the "rudder-drive" system stability. The rudder flutter represents a dynamic form of
V. N. Akimov +3 more
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Research on the Motion Characteristics of Longitudinal Second Fold Wings [PDF]
Hangkong bingqi, 2023 Folding wings are flight device structural components that require small space for ammunition seeking, facilitating the storage and transportation of launch boxes (barrels), greatly saving ammunition storage and transportation space, and increasing the ...
Lü Tiegang, Zhang Xiaowen, Li Yongwei, Zhang Yu
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