๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Analysis of limit cycle oscillations of a typical airfoil section with freeplay

โœ Scribed by Zhang, Si-Jin; Wen, Gui-Lin; Peng, Fan; Liu, Zi-Qiang


Book ID
120999462
Publisher
The Chinese Society of Theoretical and Applied Mechanics; Institute of Mechanics, Chinese Academy of Sciences
Year
2013
Tongue
English
Weight
552 KB
Volume
29
Category
Article
ISSN
0567-7718

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


NONLINEAR BEHAVIOR OF A TYPICAL AIRFOIL
โœ M.D. Conner; D.M. Tang; E.H. Dowell; L.N. Virgin ๐Ÿ“‚ Article ๐Ÿ“… 1997 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 494 KB

A three degree-of-freedom aeroelastic typical section with control surface freeplay is modeled theoretically as a system of piecewise linear state-space models . The system response is determined by time marching of the governing equations using a standard Runge -Kutta algorithm in conjunction with

AEROELASTIC ANALYSIS OF A FLEXIBLE AIRFO
โœ S.-H. Kim; I. Lee ๐Ÿ“‚ Article ๐Ÿ“… 1996 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 761 KB

A two-dimensional flexible airfoil with a freeplay non-linearity in pitch has been analyzed in the subsonic flow range. Structurally, the airfoil is modelled as finite beam elements and two spring elemens in pitch and plunge. A doublet lattice method is used for the two-dimensional unsteady aerodyna

LIMIT CYCLE BEHAVIOR OF AN AIRFOIL WITH
โœ D. TANG; E.H. DOWELL; L.N. VIRGIN ๐Ÿ“‚ Article ๐Ÿ“… 1998 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 448 KB

A three-degree-of-freedom aeroelastic model with freeplay is modeled theoretically using a small number of aerodynamic eigenmodes (i.e. a reduced order model) based upon Peters' finite-state model for two-dimensional aerodynamic flow. The limit cycle behavior and the sensitivity to initial condition