Horizontal axis wind turbine research: A review of commercial CFD, FE codes and experimental practices

JM O'Brien, TM Young, DC O'Mahoney… - Progress in Aerospace …, 2017 - Elsevier
A review of wind turbine aerodynamics research is presented. The review is limited to
Horizontal Axis Wind Turbine (HAWT) investigations. The focus is on recent near wake …

Thin-walled beams made of functionally graded materials and operating in a high temperature environment: vibration and stability

L Librescu, SY Oh, O Song - Journal of Thermal Stresses, 2005 - Taylor & Francis
In this study, problems related to the thermoelastic modeling and behavior of thin-walled
beams made of functionally graded materials (FGMs) are addressed. In this context, two …

Nonlinear dynamic analysis of parked large wind turbine blade considering harmonic inertial excitation using continuum mathematical model

B Jiang, Y Hui, Q Yang, X Hua - Thin-Walled Structures, 2022 - Elsevier
In this paper, an investigation on the nonlinear dynamics of parked large wind turbine
blades considering harmonic inertial excitation is presented. The investigation is based on …

Observer-Based Adaptive Control for a Coupled PDE–ODE System of a Flexible Wing

T Meng, Y Zhang, Q Fu, J Wang - IEEE Transactions on …, 2024 - ieeexplore.ieee.org
This article proposes an adaptive observer-based control to address the PDE–ODE coupled
system of a flexible wing, where external disturbances and references have unknown …

An experimental-theoretical correlation study of non-linear bending and torsion deformations of a cantilever beam

EH Dowell, J Traybar, DH Hodges - Journal of Sound and Vibration, 1977 - Elsevier
An experimental study of the large deformation of a cantilevered beam under a gravity tip
load has been made. The beam root is rotated so that the tip load is oriented at various …

Rotorcraft comprehensive code assessment for blade–vortex interaction conditions

M Gennaretti, G Bernardini, J Serafini… - Aerospace Science and …, 2018 - Elsevier
The scope of this paper is the presentation of the computational methodologies applied in
the comprehensive code for rotorcraft developed in the last years at Roma Tre University …

Modeling particle spray and capture efficiency for direct laser deposition using a four nozzle powder injection system

C Katinas, W Shang, YC Shin… - Journal of …, 2018 - asmedigitalcollection.asme.org
Powder capture efficiency is indicative of the amount of material that is added to the
substrate during laser additive manufacturing (AM) processes, and thus, being able to …

Recent developments in the dynamics of advanced rotor systems

W Johnson - 1985 - ntrs.nasa.gov
The problems that were encountered in the dynamics of advanced rotor systems are
described. The methods for analyzing these problems are discussed, as are past solutions …

Analysis of a structural-aerodynamic fully-coupled formulation for aeroelastic response of rotorcraft

G Bernardini, J Serafini, MM Colella… - Aerospace Science and …, 2013 - Elsevier
This paper deals with a computational aeroelastic tool aimed at the analysis of the response
of rotary wings in arbitrary steady motion. It has been developed by coupling a nonlinear …

Coupled nonlinear aeroelasticity and flight dynamics of fully flexible aircraft

W Su - 2008 - search.proquest.com
This dissertation introduces an approach to effectively model and analyze the coupled
nonlinear aeroelasticity and flight dynamics of highly flexible aircraft. A reduced-order …