A previous work of the authors shows that a cantilever skew plate acted upon by an aerodynamic force and a small, slowly varying in-plane force may become unstable before the aerodynamic force reaches its critical value. This paper describes a study of the non-linear vibration of a cantilever skew p
AERODYNAMIC DAMPING OF RANDOMLY EXCITED PLATES IN STATIONARY AND MOVING AIR
โ Scribed by A.Z. TARNOPOLSKY; J.C.S. LAI; N.H. FLETCHER
- Publisher
- Elsevier Science
- Year
- 2002
- Tongue
- English
- Weight
- 207 KB
- Volume
- 253
- Category
- Article
- ISSN
- 0022-460X
No coin nor oath required. For personal study only.
โฆ Synopsis
An experimental study of the aerodynamic damping of oscillating plates has been undertaken. Plates of various shapes were placed into an air #ow normal to the plate and excited to oscillate parallel to the #ow direction by electromagnetic forces of equal amplitudes and random frequencies. The aerodynamic damping of oscillating plates, evaluated in terms of a quality Q-factor from a frequency response resonance curve, was found to vary linearly with the absolute pressure in stationary surrounding air and with the air #ow velocity in moving air. The #ow velocity was also found to a!ect the aerodynamic damping more than the absolute pressure. A simple empirical model has been developed to predict the variation of the aerodynamic damping with the #ow velocity.
๐ SIMILAR VOLUMES
The investigation reported in this paper constitutes the second phase of an on-going research project that aims at developing techniques for the computation and analysis of response of complex structures excited by non-parametric and parametric non-stationary random disturbances. In this second phas