@inproceedings{oai:jaxa.repo.nii.ac.jp:00005662,
 author = {Balakrishnan, A. V.},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling},
 month = {Feb},
 note = {Using full continuum models, we establish purely theoretically that in two-dimensional isentropic flow, the flutter speed for a slender high-aspect ratio wing is a Hopf bifurcation point of the aeroelastic structure dynamics which can be expressed as a non-linear convolution evolution equation. The flutter speed is determined by the linearized model and the LCO (Limit Cycle Oscillation) is periodic with period (2 pi/omega) where omega is the angular flutter frequency in the linear model, and can be expressed as a harmonic series., 資料番号: AA0063824007, レポート番号: JAXA-SP-07-008E},
 pages = {64--76},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Flutter LCO in isentropic flow: Analytical theory},
 volume = {JAXA-SP-07-008E},
 year = {2008}
}