AIAA Journal, volume 55, issue 10, pages 3499-3516

Transonic Panel Flutter Predictions Using a Linearized Stability Formulation

Manav Bhatia ¹

Philip Beran ²

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Mississippi State University, Mississippi State, Mississippi 39762 |

U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Dayton, Ohio 45433 |

Publication type: Journal Article

Publication date: 2017-09-06

American Institute of Aeronautics and Astronautics (AIAA)

Journal: AIAA Journal

scimago Q1

SJR: 1.023

CiteScore: 5.6

Impact factor: 2.1

ISSN: 00011452, 1533385X

DOI: 10.2514/1.j055839

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Aerospace Engineering

Abstract

A methodology is presented for prediction of dynamic instabilities arising from fluid–structure coupling. The inviscid compressible Euler equations are linearized about a steady-state solution and ...

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Elsevier	Elsevier, 7, 41.18% Elsevier 7 publications, 41.18%
American Institute of Aeronautics and Astronautics (AIAA)	American Institute of Aeronautics and Astronautics (AIAA), 7, 41.18% American Institute of Aeronautics and Astronautics (AIAA) 7 publications, 41.18%
MDPI	MDPI, 1, 5.88% MDPI 1 publication, 5.88%
Springer Nature	Springer Nature, 1, 5.88% Springer Nature 1 publication, 5.88%
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Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Journal

AIAA Journal

scimago Q1

SJR

1.023

CiteScore

5.6

Impact factor

2.1

ISSN

00011452 (Print)

1533385X (Electronic)

Transonic Panel Flutter Predictions Using a Linearized Stability Formulation

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