ARTICLES

Filter  
Active filters 0
Remove
  

Refine your searches by:

Collections
Mechanical Engineering
Hydraulic engineer
Mathematics
Pure sciences
Physical
Environmental engineering
Civil Engineering
Industrial engineer
Research
Transport
all records (13)

Languages
English

Countries
USA
Italy
Spain
Malaysia
Czech Republic
Germany
Switzerland

Years
2019
2018
2017
2016
2015
2014
2012
2011
2006
2004

Filter  
 
19  Articles
1 of 3 pages  |  10  records  |  more records»
One of many problems in the field of sailplane design is that of aeroelastic stability. Practicing designers of gliders and light aircraft seldom have the opportunity to spend a great deal of time studying the difficult background of flutter. Therefore, t... see more

This paper demonstrates the implementation of an adaptive feedforward controller to reduce structural vibrations on a wing typical section. The aeroelastic model includes a structural nonlinearity, which is modelled in a polynomial form. Aeroelastic vibra... see more

This work discusses the quantitative stability evaluation of aeroelastic problems withfreeplay in the control surfaces. Stability estimation of linear time invariant and linear timeperiodic systems rely on eigenanalysis of state transition matrices and im... see more

This work addresses the involuntary interaction between the pilot and the vehicle, with specific reference to helicopters along the vertical (or heave) axis. The problem is described and formulated mathematically. Means of analysis are discussed. Focus is... see more

This paper focuses on the computational study of nonlinear effects of unsteady aerodynamics for non-classical aileron buzz. It aims at a comprehensive investigation of aileron buzz phenomenon under varying flow parameters utilizing the classical approach ... see more

In this paper a tool, previously developed and validated for the prediction of wing box structural weight in very early design stages, is improved to better match effects on panel sizing of stability constraints. It is applied to an unconventional configu... see more

-

-

ABSTRACT: Flutter may be considered to be one of the most dangerous aeroelastic failure phenomenon. The flutter characteristic differs for each aircraft type, and depends on the wing geometry as well as its operational region of subsonic, transonic or sup... see more

1 of 3 pages  |  10  records  |  more records»