Engineering Applications of Computational Fluid Mechanics, 2019 In this paper, optimization of the first blade of a new test rig is pursued using a hybrid model comprising the genetic algorithm, artificial neural networks and design of experiments.
Mohammad Ghalandari +5 more
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Performance Evaluation of Stator-Rotor Cascade System Considering Flow Viscosity and Aeroelastic Deformation Effects [PDF]
, 2008 Dong-Hyun Kim
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EnergiesThis paper investigates the aeroelastic behaviour of a full wind turbine model with realistic blade vibration amplitude (9% span) using a nonlinear frequency-domain solution method.
Shine Win Naung +2 more
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Dynamic similarity criteria for simple cases of buildings and structures aerodynamics
Budownictwo i ArchitekturaThe work concerns dynamic similarity criteria of various phenomena occurring in hydraulics and fluid dynamics originally derived from ratios of forces and forces moments affecting these phenomena. The base of dynamic similarity criteria formulations and
Andrzej Flaga, Łukasz Flaga
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A Time-Domain Calculation Method for Gust Aerodynamics in Flight Simulation
AerospaceGusts have a significant impact on aircraft and need to be analyzed through flight simulations. The solution for time-domain gust aerodynamic forces stands as a pivotal stage in this process. With the increasing demand for flight simulations within gusty
Zexuan Yang +4 more
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Modeling and analysis of high aspect ratio wing considering random structural parameters. [PDF]
Sci Rep, 2021 Fu B, Yang Y, Qi H, Xu J, Wang S.
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Surrogate-based aeroelastic design optimization of tip extensions on a modern 10 MW wind turbine [PDF]
, 2021 Thanasis Barlas +3 more
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THE STUDY OF THE STABILITY OF AEROELASTIC SYSTEMS BY LINEAR APPROXIMATION
, 2020 Iulia V. Pokladova, Petr A. Velmisov
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VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
Научный вестник МГТУ ГА, 2016 The results of computational and experimental study of thin wings flutter in separated and unseparated flow are presented. The effect of flutter suppressing in the presence of separation is found.
V. V. Ovchinnikov, Yu. V. Petrov
doaj
Dataset of numerical simulations for aeroelastic control of an aero engine compressor cascade using plasma actuators. [PDF]
Data Brief, 2021 De Giorgi MG +3 more
europepmc +1 more source