Dynamic stability of cantilevered timoshenko columns subjected to a rocket thrust

Computers and Structures

Volumn 51, Issue 4, 1994, Pages 331-335

  Ryu, B J ^a   Sugiyama, Y ^b  

^a Daejon Health Institute of Technology   (South Korea)

^b Osaka Prefecture University   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BEAMS AND GIRDERS; DEFORMATION; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; LOADS (FORCES); MATHEMATICAL MODELS; ROCKET ENGINES; SHEAR STRESS; SPACECRAFT; STABILITY;

CANTILEVERED TIMOSHENKO COLUMNS; DYNAMIC STABILITY; EXTENDED HAMILTON'S PRINCIPLE; ROTARY INERTIA PARAMETER; SOLID ROCKET MOTOR; THRUST FORCE;

COLUMNS (STRUCTURAL);

EID: 0028427103     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/0045-7949(94)90318-2     Document Type: Article

References (9)

1. Die Knicklast des Einseitig Eingespannten Tangential gedrückten Stabes
2. Stability of tapered cantilever columns subjected to follower forces
3. Influence of boundary conditions on the stability of a column under non-conservative load
4. The maximum controlled follower force on a free-free beam carrying a concentrated mass
5. Experiment on flutter of cantilevered columns subjected to a rocket thrust
6. Stability analysis of a Timoshenko beam subjected to distributed follower forces using finite elements
7. Eigenvalue sensitivity in the stability analysis of Beck's column with a concentrated mass at the free end
8. Vibration and stability of clamped-elastically restrained Timoshenko column under nonconservative load
9. The effect of two concentrated masses on the dynamic stability of a free-free Timoshenko beam subjected to a follower force