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The effect of section model details on aeroelastic parameters

✍ Scribed by N.P. Jones; R.H. Scanlan; P.P. Sarkar; L. Singha


Publisher
Elsevier Science
Year
1995
Tongue
English
Weight
421 KB
Volume
54-55
Category
Article
ISSN
0167-6105

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This paper deals with the aeroelastic instability and non-linear post-critical behaviour of a two degree-of-freedom oscillatory system. The main goal of the study is an introduction of a realistic nonlinear theoretical model making possible a detailed non-linear analysis of post-critical states of a