首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Nonlinear aeroelastic analysis of airfoils: bifurcation and chaos
Institution:1. Aerodynamics Laboratory, Institute for Aerospace Research, National Research Council, Ottawa, Ontario, Canada K1A 0R6;2. Department of Mechanical Engineering, McGill University, Montreal, Quebec, Canada H3A 2K6;3. Department of Mathematical Sciences, University of Alberta, Edmonton, Alberta, Canada T6G 2G1;1. Department of Applied Mechanics, Indian Institute of Technology Madras, Chennai 600036, India;2. Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India;1. Centre for Aeronautics, Cranfield University, Cranfield, Bedfordshire MK43 0AL, UK;2. School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, People’s Republic of China
Abstract:Different types of structural and aerodynamic nonlinearities commonly encountered in aeronautical engineering are discussed. The equations of motion of a two-dimensional airfoil oscillating in pitch and plunge are derived for a structural nonlinearity using subsonic aerodynamics theory. Three classical nonlinearities, namely, cubic, freeplay and hysteresis are investigated in some detail. The governing equations are reduced to a set of ordinary differential equations suitable for numerical simulations and analytical investigation of the system stability. The onset of Hopf-bifurcation, and amplitudes and frequencies of limit cycle oscillations are investigated, with examples given for a cubic hardening spring. For various geometries of the freeplay, bifurcations and chaos are discussed via the phase plane, Poincaré maps, and Lyapunov spectrum. The route to chaos is investigated from bifurcation diagrams, and for the freeplay nonlinearity it is shown that frequency doubling is the most commonly observed route. Examples of aerodynamic nonlinearities arising from transonic flow and dynamic stall are discussed, and special attention is paid to numerical simulation results for dynamic stall using a time-synthesized method for the unsteady aerodynamics. The assumption of uniform flow is usually not met in practice since perturbations in velocities are encountered in flight. Longitudinal atmospheric turbulence is introduced to show its effect on both the flutter boundary and the onset of Hopf-bifurcation for a cubic restoring force.
Keywords:
本文献已被 ScienceDirect 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号