THE HYDROELASTIC STABILITY OF 3-DIMENSIONAL DISTURBANCES OF A FINITE COMPLIANT WALL

被引:43
作者
LUCEY, AD
CARPENTER, PW
机构
[1] Department of Engineering, University of Warwick, Coventry
关键词
D O I
10.1006/jsvi.1993.1275
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
A theoretical investigation of the hydroelastic behaviour of a compliant panel of finite dimensions is presented. The mechanics of the wall are modelled by using a linear differential operator with a single degree of freedom, and the results herein pertain to a spring-backed flexible plate. Unsteady potential flow is assumed; thus, the onset of divergence instability defines the critical flow speed. At higher flow speeds, this static instability may give way to modal coalescence flutter which takes the form of a downstream travelling wave. Comparison is made between the present analysis and an equivalent two-dimensional (infinite width) study for a compliant wall of finite length. It is demonstrated that the simpler two-dimensional methods of instability prediction are always appropriate when the aspect ratio is greater than five. Increasing the streamwise mode number (i.e., reducing the ratio of disturbance wavelength to panel length) renders the system progressively more two-dimensional in its behaviour. The order of the critical mode is promoted by increasing the foundation-spring stiffness, reducing the width of the panel or imposing a higher order transverse mode than the fundamental. For a compliant panel of prescribed surface area, a critical aspect ratio exists in which configuration the lowest divergence-onset flow speed is found. Arrays of compliant panels are considered: the influence of neighbouring panels exercises a mildly adverse effect on the stability of a panel in a comparison with the response of a similar panel in isolation. © 1993 Academic Press Limited.
引用
收藏
页码:527 / 552
页数:26
相关论文
共 36 条
[11]  
DUGUNDJI J, 1963, AM I AERONAUTICS AST, V11, P1146
[12]   NONLINEAR STABILITY OF PANELS IN INCOMPRESSIBLE-FLOW [J].
ELLEN, CH .
JOURNAL OF SOUND AND VIBRATION, 1977, 54 (01) :117-121
[13]   STABILITY OF SIMPLY SUPPORTED RECTANGULAR SURFACES IN UNIFORM SUBSONIC FLOW [J].
ELLEN, CH .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1973, 40 (01) :68-72
[14]   STABILITY OF AN ISOLATED RECTANGULAR SURFACE EMBEDDED IN UNIFORM SUBSONIC FLOW [J].
ELLEN, CH .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1977, 44 (02) :201-206
[15]   STABILITY OF CLAMPED RECTANGULAR PLATES IN UNIFORM SUBSONIC FLOW [J].
ELLEN, CH .
AIAA JOURNAL, 1972, 10 (12) :1716-1717
[16]   ON THE INTERACTION OF COMPLIANT COATINGS WITH BOUNDARY-LAYER FLOWS [J].
GADELHAK, M ;
BLACKWELDER, RF ;
RILEY, JJ .
JOURNAL OF FLUID MECHANICS, 1984, 140 (MAR) :257-280
[17]   ON THE AERODYNAMIC FORCES INVOLVED IN AEROELASTIC INSTABILITY OF TWO-DIMENSIONAL PANELS IN UNIFORM INCOMPRESSIBLE-FLOW [J].
GARRAD, AD ;
CARPENTER, PW .
JOURNAL OF SOUND AND VIBRATION, 1982, 80 (03) :437-439
[18]  
GARRAD AD, 1980, THESIS U EXETER
[19]  
GARRAD AD, 1982, J SOUND VIBRATION, V84, P483
[20]  
Gaster M., 1987, P IUTAM S TURB MAN R, P285