Unsteady Lifting-Line Free-Wake Aerodynamic Modeling for Morphing Wings
AerospaceA time-stepping, lifting-line solution algorithm for the prediction of the unsteady aerodynamics of morphing wings is presented. The velocity induced by the wake vorticity is determined through a free-wake vortex-lattice model, whereas the Küssner and ...
Gregorio Frassoldati +3 more
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THE DISCRETE VORTEXES METHOD WITH THE IMPROVED QUADRATURE FORMULAE IN THE AEROELASTICITY PROBLEMS
Научный вестник МГТУ ГА, 2016 The possibility of the improved quadrature formulae of the discrete vortexes method used in the aeroelasticity problems is considered. Some of the calculation results confirm the efficiency of these formulae are carried out.
V. V. Ovchinnicov +2 more
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Numerical Simulation of Folding Tail Aeroelasticity Based on the CFD/CSD Coupling Method
VibrationThis paper presents a CFD/CSD coupling method for aeroelastic simulation of folding tail morphing aircraft. The unsteady aerodynamic analysis is based on an in-house computational fluid dynamics (CFD) solver for the Euler equations, and emphasis is made ...
Di Zhou +6 more
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Assessment of the Fatigue Behavior of Wings with Distributed Propulsion
Engineering ProceedingsThe integration of distributed electric propulsion into a wing significantly alters the dynamic behavior of the wing. Consequently, the loads on the wing structure in service, in particular upon transient gust and landing impact loads, change ...
Lukas Kettenhofen +2 more
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Numerical and Experimental Methods for the Assessment of Wind Turbine Control Upgrades
Applied Sciences, 2018 Megawatt-scale wind turbine technology is nowadays mature and, therefore, several technical improvements in order to optimize the efficiency of wind power conversion have been recently spreading in the industry.
Davide Astolfi +3 more
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THE COMPLEX OF STANDS FOR TESTING THE AIR CUSHION CHASSIS OF AIRCRAFT AND VEHICLES
Научный вестник МГТУ ГА, 2016 This article deals with a set of stands made in NIMK TSAGI for testing and creating the air cushion chassis for the aircraft and vehicles. It allows to fully embrace the process of developing and constructing the air cushion chassis for aircraft and ...
V. A. Brusov +3 more
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Thermal Aeroelastic Tailoring for Laminated Panel with Lamination Parameters and JAYA Algorithm [PDF]
, 2022 Peng Jin, Qihao Zheng, Wei Wei
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Low-Engine-Order Forced Response Analysis of a Turbine Stage with Damaged Stator Vane. [PDF]
Entropy (Basel), 2023 Zheng Y, Jin X, Yang H.
europepmc +1 more source
Numerical and experimental studies of aeroelastic hinged wingtips [PDF]
, 2023 Davide Balatti
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A Study on the Surrogate-Based Optimization of Flexible Wings Considering a Flutter Constraint
Applied SciencesAccounting for aeroelastic phenomena, such as flutter, in the conceptual design phase is becoming more important as the trend toward increasing the wing aspect ratio forges ahead. However, this task is computationally expensive, especially when utilizing
Alessandra Lunghitano +2 more
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