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Cited by 35 publications
(21 citation statements)
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“…1 Marques et al demonstrated the significant impact of structural variability on transonic flutter predictions. 2,3 When nonlinearities are present, the amplitude of oscillations can become limited and limit cycle oscillations are observed. This is a problem of considerable practical interest and is well documented for in-service aircraft.…”
Section: Introductionmentioning
confidence: 99%
“…1 Marques et al demonstrated the significant impact of structural variability on transonic flutter predictions. 2,3 When nonlinearities are present, the amplitude of oscillations can become limited and limit cycle oscillations are observed. This is a problem of considerable practical interest and is well documented for in-service aircraft.…”
Section: Introductionmentioning
confidence: 99%
“…The wing is divided into three regions: root, pylon, and tip. To match the natural frequencies of the FE model to those found for the symmetric modes in the GVT [26], Young's modulus and density of each region of the wing are considered as updating parameters [27,28]. Full information on structural properties, based on those of aluminium, and the mapping of modes to the fluid surface grid, are given in [31].…”
Section: Open Source Fighter (Osf)mentioning
confidence: 99%
“…Furthermore, predicting the aeroelastic stability of an aircraft should also identify the consequences of variability or uncertainty in model parameters, as discussed by Pettit [2]. Marques et al demonstrated the significant impact of structural variability on transonic flutter predictions [3,4]. When nonlinearities are present, the amplitude of oscillations can become limited and limit cycle oscillations are observed.…”
Section: Introductionmentioning
confidence: 99%