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Method for Flutter Aeroservoelastic Open Loop Analysis

[+] Author Affiliations
Ruxandra Botez, Alexandre Doin, Iulian Cotoi

Ecole de Technologie Supérieure, Montreal, Quebec, Canada

Paper No. IMECE2002-33623, pp. 547-558; 12 pages
doi:10.1115/IMECE2002-33623
From:
  • ASME 2002 International Mechanical Engineering Congress and Exposition
  • 5th International Symposium on Fluid Structure Interaction, Aeroelasticity, and Flow Induced Vibration and Noise
  • New Orleans, Louisiana, USA, November 17–22, 2002
  • Conference Sponsors: Applied Mechanics Division
  • ISBN: 0-7918-3659-2 | eISBN: 0-7918-1691-5, 0-7918-1692-3, 0-7918-1693-1
  • Copyright © 2002 by ASME

abstract

Aeroservoelasticity (ASE) is a multidisciplinary study of interactions between structural dynamics, unsteady aerodynamics and control systems. In this paper, the Aircraft Test Model ATM developed by NASA Dryden Flight Research Center is used, and the velocities at which flutter occurs are calculated by use of the STARS aeroservoelastic software. For the validation of our aeroservoelastic study, STARS aeroservoelastic software developed also by NASA is used. We develop a new aeroservoelastic tool in Matlab to consider these interactions, and the obtained results through our method are compared to the ones obtained in STARS.

Copyright © 2002 by ASME

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