Resolvent Analysis for Flutter Boundary Prediction in Transonic Flow-Reference-Cited by-同舟云学术

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Resolvent Analysis for Flutter Boundary Prediction in Transonic Flow

Published:2024-07-01 Issue: Volume: Page:1-5
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Yuan Hao¹,Kou Jiaqing¹^ORCID,Gao Chuanqiang¹,Zhang Weiwei¹

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Innovative Research Group Project of the National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J064214

Reference27 articles.

1. MODELING OF FLUID-STRUCTURE INTERACTION

2. TheodorsenT. “General Theory of Aerodynamic Instability and the Mechanism of Flutter,” NACA TR-496, 1949.

3. Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations

4. Calculation of Transonic Aileron Buzz

5. Linearized Euler predictions of unsteady aerodynamic loads in cascades

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