An overview on the use of unmanned aerial vehicles for medical product transportation: flight dynamics and vibration issues

RS Geronel, GR Begnini, RM Botez… - Journal of the Brazilian …, 2022 - Springer
Advances in technology and the possibility to carry different sensors and payloads have led
to the increasing use of unmanned aerial vehicles (UAVs) by the medical sector. Currently …

Exact eigensolutions for flutter of two-dimensional symmetric cross-ply composite laminates at high supersonic speeds

Q Sun, Y **ng - Composite Structures, 2018 - Elsevier
Exact eigensolutions for flutter of two-dimensional (2D) symmetric cross-ply composite
laminated panel with all combinations of simply supported (S), guided (G), clamped (C) and …

An aeroelastic beam finite element for time domain preliminary aeroelastic analysis

CR Vindigni, G Mantegna, A Esposito… - Mechanics of …, 2023 - Taylor & Francis
An aeroelastic beam finite element based on Euler-Bernoulli beam theory and two-
dimensional unsteady aerodynamics is presented. Based on the flexural-torsional equations …

Three-dimensional flutter analysis of a novel circular sandwich plate employing hyperbolic shear deformation theory

R Aboutalebi - Aerospace Science and Technology, 2024 - Elsevier
Abstract Magnetorheological elastomers (MREs) Characterize a category of intelligent
materials renowned for their distinct responsiveness to external magnetic fields …

[HTML][HTML] Assessing the retrieval procedure of complex-valued forces from airborne pressure fields by means of DIC-based full-field receptances in simplified pseudo …

A Zanarini - Aerospace Science and Technology, 2025 - Elsevier
Lightweight structural components in many engineering fields can be severely excited by
airborne pressure fields, becoming a concern for their structural dynamics and reliability …

Aeroelastic flutter analysis considering modeling uncertainties

M Lokatt - Journal of fluids and structures, 2017 - Elsevier
A method for efficient flutter analysis of aeroelastic systems including modeling uncertainties
is presented. The aerodynamic model is approximated by a piece-wise continuous rational …

A reduced order state space model for aeroelastic analysis in time domain

CR Marqui, DD Bueno, LCS Goes… - Journal of Fluids and …, 2017 - Elsevier
The objective of this paper is to describe a new method for modeling aeroelastic system in
time domain based on a modification of the Laguerre Polynomials to represent complex …

A new look at the Equivalent Linearization Technique to predict LCO in aeroelastic systems with discrete nonlinearities

LD Wayhs-Lopes, EH Dowell, DD Bueno - Journal of Fluids and Structures, 2023 - Elsevier
Control surfaces nonlinearities can lead to limit cycle oscillations (LCO). Several methods
have been proposed to predict LCO, such as Harmonic Balance-based methods (HB) …

A successive robust flutter prediction technique for aeroelastic systems using µ method

AK Onkar - Meccanica, 2021 - Springer
In this work, a successive robust flutter prediction technique is developed by coupling
nominal analysis, ground vibration test, wind tunnel test, uncertainty model updation and …

Frequency domain approach for probabilistic flutter analysis using stochastic finite elements

S Kumar, AK Onkar, M Maligappa - Meccanica, 2019 - Springer
In this work, a stochastic finite element method based on first order perturbation approach is
developed for the probabilistic flutter analysis of aircraft wing in frequency domain. Here …