Results 1 to 10 of about 511 (182)

Nonlinear Aeroelastic Simulations and Stability Analysis of the Pazy Wing Aeroelastic Benchmark [PDF]

open access: yesAerospace, 2021
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
doaj   +3 more sources

Influence of structure parameters on aeroelastic stability for labyrinth seal based on energy method

open access: yesPropulsion 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
doaj   +3 more sources

Parametric Study of Aeroelastic Instability Boundaries of Space Launch Vehicle in Subsonic Flow [PDF]

open access: yesفصلنامه علوم و فناوری فضایی, 2022
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
doaj   +1 more source

Aero-Elastic Stability of Horizontal Axis Wind Turbine Blades [PDF]

open access: yesRenewable Energy Research and Applications, 2021
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
doaj   +1 more source

Time-domain Analytical Method for Aeroelastic Analysis of High Aspect Ratio Wing Using Unsteady Indicial Aerodynamics [PDF]

open access: yesINCAS Bulletin, 2022
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
doaj   +1 more source

Aeroelastic Tailoring of the Next Generation Civil Tiltrotor Technological Demonstrator Composite Wing

open access: yesAerospace, 2022
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
doaj   +1 more source

Aeroelastic analysis and flutter control of wings and panels: A review

open access: yesInternational Journal of Mechanical System Dynamics, 2021
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
doaj   +1 more source

Quantitative Aeroelastic Stability Prediction of Wings Exhibiting Nonlinear Restoring Forces

open access: yesJournal of Mathematical Sciences and Modelling, 2023
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
doaj   +1 more source

Aeroelastic vibration analysis of a 1.5 stage compressor

open access: yesPropulsion and Power Research, 2020
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
doaj   +1 more source

Aeroelastic Stability Analysis of Electric Aircraft Wings with Distributed Electric Propulsors

open access: yesAerospace, 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
doaj   +1 more source

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