New Robust Method to Study Flight Flutter Testing-Reference-Cited by-同舟云学术

New Robust Method to Study Flight Flutter Testing

Published:2019-01 Issue:1 Volume:56 Page:336-343
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Le Clainche Soledad¹,Moreno-Ramos Rubén²,Taylor Paul³,Vega José M.¹

Affiliation:

1. Polytechnic University of Madrid, E-28040 Madrid, Spain

2. Altran Innovación, E-28022 Madrid, Spain

3. Gulfstream Aerospace, Savannah, Georgia 31402

Funder

Spanish Ministry of Economy and Competitiveness

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034863

Reference32 articles.

1. Identification of aeroelastic parameters using a recursive sequential least squares method

2. Flight Flutter Test and Data Analysis Techniques Applied to a Drone Aircraft

3. Method for experimental determination of flutter speed by parameter identification

4. CooperJ. “Parameter Estimation Methods for Flight Flutter Testing,” Proceedings of the 80th AGARD Structures and Materials Panel, AGARD CP-566, Neuilly-Sur-Seine, France, 1995, pp. 10.1–10.12.

5. BrennerM. J.LindR. C.VoracekD. F. “Overview of Recent Flight Flutter Testing Research at NASA Dryden,” NASA TM 4792, April 1997.

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