Structural dynamic reanalysis method for transonic aeroelastic analysis with global structural modifications-Reference-Cited by-同舟云学术

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Structural dynamic reanalysis method for transonic aeroelastic analysis with global structural modifications

Published:2017-10 Issue: Volume:74 Page:306-320
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Li Dongfeng,Zhou Qiang,Chen Gang,Li Yueming

Funder

National Natural Science Foundation of China

National Key Foundation

Shaanxi Natural Science Foundation

Central Universities

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference46 articles.

1. Fast exact linear and non-linear structural reanalysis and the sherman–morrison–woodbury formulas;Akgün;Internat. J. Numer. Methods Engrg.,2001

2. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows;Albano;AIAA J.,1969

3. Role of shocks in the “sub-transonic” flutter phenomenon;Ashley;J. Aircr.,1980

4. Piston theory, a new aerodynamic tool for the aeroelastican;Ashley;J. Aeronaut. Sci.,1956

5. Iterative least-squares calculation for modal eigenvector sensitivity;Beliveau;AIAA J.,1996

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