Reduced-Order Nonlinear Damping Model: Formulation and Application to Postflutter Aeroelastic Behavior-Reference-Cited by-同舟云学术

Reduced-Order Nonlinear Damping Model: Formulation and Application to Postflutter Aeroelastic Behavior

Published:2021-10 Issue:10 Volume:59 Page:4144-4154
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Wang X. Q.¹,Song Pengchao¹,Mignolet Marc P.¹,Chen P. C.²

Affiliation:

1. Arizona State University, Tempe, Arizona 85287

2. ZONA Technology, Scottsdale, Arizona 85258

Funder

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J059804

Reference20 articles.

1. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores

2. Application of a three-field nonlinear fluid–structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter

3. ParanantaB. B.KokJ. C.SpekreijseS. P.HounjetM. H. L.MeijerJ. J. “Simulation of Limit Cycle Oscillation of Fighter Aircraft at Moderate Angle of Attack,” National Aerospace Lab./NLR TP 2003-526, Amsterdam, 2003, pp. 1–38, https://reports.nlr.nl/xmlui/bitstream/handle/10921/644/TP-2003-526.pdf?sequence=1&isAllowed=y [retrieved 2021].

4. A review of indirect/non-intrusive reduced order modeling of nonlinear geometric structures

5. Nonlinear reduced order modeling of isotropic and functionally graded plates

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