Nonlinear Aeroelastic Simulations and Stability Analysis of the Pazy Wing Aeroelastic Benchmark [PDF]
The Pazy wing aeroelastic benchmark is a highly flexible wind tunnel model investigated in the Large Deflection Working Group as part of the Third Aeroelastic Prediction Workshop.
Jonathan Hilger, Markus Raimund Ritter
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Influence of structure parameters on aeroelastic stability for labyrinth seal based on energy method
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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Parametric Study of Aeroelastic Instability Boundaries of Space Launch Vehicle in Subsonic Flow [PDF]
In the present work, the frequency-domain aeroelastic stability analysis of space launch vehicle body in the flight condition of initial launch phase is presented for a range of geometric parameters, structural characteristics, and other parameters such ...
Armin Azodi +2 more
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Aero-Elastic Stability of Horizontal Axis Wind Turbine Blades [PDF]
Multi-Megawatt wind turbines have long, slender and heavy blades that can undergo extremely wind loadings. Aeroelastic stability of wind turbine blades is of great importance in both power production and load carrying capacity of structure.
Seyyed A. Sina
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Time-domain Analytical Method for Aeroelastic Analysis of High Aspect Ratio Wing Using Unsteady Indicial Aerodynamics [PDF]
This paper deals with the development of a novel time-domain analytical method to perform an aeroelastic stability analysis of a high aspect ratio wing. The aerodynamic model in this paper is built upon the frequency domain of Theodorsen aerodynamics. An
Zia Ur REHMAN
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The tiltrotor wing structure is one of the most critical and heavily investigated structures in design due to the fundamental need to consider the interactions between the wing, pylon, and rotor systems to achieve aircraft aeroelastic stability.
Aniello Daniele Marano +8 more
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Aeroelastic analysis and flutter control of wings and panels: A review
Flutter is a self‐excited vibration under the interaction of the inertial force, aerodynamic force, and elastic force of the structure. After the flutter occurs, the aircraft structures will exhibit limit cycle oscillation, which will cause catastrophic ...
Yuyang Chai +4 more
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Quantitative Aeroelastic Stability Prediction of Wings Exhibiting Nonlinear Restoring Forces
In engineering practice, eigen-solution is used to assess the stability of linear dynamical systems. However, the linearity assumption in dynamical systems sometimes implies simplifications, particularly when strong nonlinearities exist.
Aykut Tamer
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Aeroelastic vibration analysis of a 1.5 stage compressor
Aeroelastic vibration problems are commonly found in modern compressors operating in off-design conditions. Large amplitude vibration could lead to high cycle fatigue (HCF) of blade and usually occurs in front stages of axial compressors.
Yun Zheng +3 more
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Aeroelastic Stability Analysis of Electric Aircraft Wings with Distributed Electric Propulsors
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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