Passive damping devices for aerospace structures

Acta Astronautica

Volumn 50, Issue 10, 2002, Pages 597-608

  Rittweger, A ^a,d   Albus, J ^a   Hornung, E ^a   Ory H ^b   Mourey, P ^c  

^a DAIMLER AG   (Germany)

^b RWTH AACHEN UNIVERSITY   (Germany)

^c CNES   (France)

^d AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; ELASTOMERS; ENERGY DISSIPATION; FRICTION; LAUNCHING; MATHEMATICAL MODELS; ORBITS; SPACECRAFT; STIFFNESS MATRIX;

AEROSPACE STRUCTURES;

AEROSPACE ENGINEERING;

EID: 0036577022     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(01)00220-X     Document Type: Article

References (6)

1. Line-of-sight performance improvement with reaction-wheel isolation
2. Application of constrained layer damping to the F/A-18 horizontal tail