INFLUENCE OF TIP MASS OFFSET ON THE STABILITY OF BECKS COLUMN

被引:1
作者
ANDERSON, GL [1 ]
VASILAKIS, JD [1 ]
WU, JJ [1 ]
机构
[1] USA, ARMAMENT RES & DEV COMMAND, BENET WEAPONS LAB, WATERVLIET ARSENAL, WATERVLIET, NY 12189 USA
关键词
D O I
10.1016/0022-460X(79)90456-5
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
In this paper, the stability of a slender cantilever carrying a tip mass at its free end and subjected there to a follower force is investigated. The centroid of the tip mass is offset from the free end of the beam and is located along its extended axis. The associated boundary value problem is solved and the exact frequency equation is derived. The frequency equation is solved numerically for the case in which both the beam and the tip mass have circular cross-sections. The numerical computations indicate that the system loses stability only through flutter. The variation of the values of the critical flutter load Qcr with the tip mass offset parameter ξ is shown graphically for four values of the tip mass density to beam density ratio p. These calculations reveal that, at sufficiently small values of ξ, Qcr decreases sharply for increasing values of p. For values of ξ sufficiently large, however, the situation is reversed as the value of Qcr increases with increasing p. © 1979.
引用
收藏
页码:475 / 480
页数:6
相关论文
共 8 条
[1]   INFLUENCE OF ROTATORY INERTIA, TIP MASS, AND DAMPING ON STABILITY OF A CANTILEVER BEAM ON AN ELASTIC FOUNDATION [J].
ANDERSON, GL .
JOURNAL OF SOUND AND VIBRATION, 1975, 43 (03) :543-552
[2]  
Beck M., 1952, ZAMM-Z ANGEW MATH ME, V3, P225, DOI DOI 10.1007/BF02008828
[3]  
Beck M., 1952, ZAMP, V3, P476
[4]   NATURAL FREQUENCIES OF A CANTILEVER WITH SLENDER TIP MASS [J].
BHAT, R ;
KULKARNI, MA .
AIAA JOURNAL, 1976, 14 (04) :536-537
[5]  
FLAX AH, 1978, AIAA J, V16, P94, DOI 10.2514/3.60864
[6]  
Pfluger A., 1955, Z ANGEW MATH MECH, V35, P191
[7]  
RAMABHAT B, 1976, J SOUND VIBRATION, V45, P304
[8]  
WALTER WW, 1968, C A S I TRANS, V1, P91