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Numerical Testing of a Trailing Edge Passive Morphing Control for Large Axial Fan Blades

[+] Author Affiliations
A. Castorrini, A. Corsini, F. Rispoli

Sapienza University of Rome, Rome, Italy

A. G. Sheard

AGS Consulting, LLLC, Atlanta, GA

Paper No. GT2017-64679, pp. V001T09A013; 11 pages
doi:10.1115/GT2017-64679
From:
  • ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition
  • Volume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards
  • Charlotte, North Carolina, USA, June 26–30, 2017
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-5077-0
  • Copyright © 2017 by ASME

abstract

The concept of morphing geometry to control and stabilize the flow has been proposed and applied in several aeronautic and wind turbine applications. We studied the effect of a similar passive system applied on an axial fan blade, analysing potential benefits and disadvantages associated to the passive coupling between fluid and structure dynamics.

The present work completes a previous study made at the section level, giving a view also on the three-dimensional effects.

We use the numerical computation to simulate the system which defines a complex fluid-structure interaction problem. In order to do that, an in-house finite element solver, already used in the previous study, is applied to solve the coupled dynamics.

Copyright © 2017 by ASME
Topics: Testing , Blades

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