Control-Surface Structural Nonlinearities in Aeroelasticity: A State of the Art Review-Reference-Cited by-同舟云学术

Control-Surface Structural Nonlinearities in Aeroelasticity: A State of the Art Review

Published:2022-06 Issue:6 Volume:60 Page:3364-3376
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Bueno Douglas D.¹^ORCID,Wayhs-Lopes Larissa D.¹^ORCID,Dowell Earl H.²

Affiliation:

1. São Paulo State University (UNESP), School of Engineering of Ilha Solteira, Ilha Solteira SP, Brazil, 15385-000

2. Duke University, Durham, North Carolina 27708-0300

Funder

Fundação de Amparo à Pesquisa do Estado de São Paulo

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J060714

Reference148 articles.

1. WoolstonD. S.RunyanH. L.ByrdsongT. A. “Some Effects of System Nonlinearities in the Problem of Aircraft Flutter,” NACA TN 3539, Oct. 1955.

2. HoffmanN.SpielbergI. “Subsonic Flutter Tests of an Unswept All-Movable Horizontal Tail,” Aircraft Laboratory, Wright Air Development Center, Air Research and Development Command, U.S. Air Force TR 54-53, Wright–Patterson Air Force Base, OH, March 1954.

3. An Investigation of Effects of Certain Types of Structural NonHnearities on Wing and Control Surface Flutter

4. TheodorsenT.GarrickI. E. “Flutter Calculations in Three Degrees of Freedom,” NACA TN 741, 1942.

5. LaurensonR. M.TrnR. M. “Flutter of Control Surfaces with Structural Nonlinearities,” U.S. Dept. of the Navy, Naval Air Systems Command, Rept. MDC E1734, Aug. 1977.

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