Modeling, vibration, and stability of elastically tailored composite thin-walled beams carrying a spinning tip rotor

Journal of the Acoustical Society of America

Volumn 110, Issue 2, 2001, Pages 877-886

  Song, Ohseop ^a   Kwon, Hyuck Dong ^b   Librescu, Liviu ^c  

^a Chungnam National University   (South Korea)

^b Yonsei University   (South Korea)

^c Virginia Polytechnic Institute and State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANISOTROPY; LIGHT; MATHEMATICAL MODELS; ROTORS; STABILITY;

EIGENVIBRATIONS;

ACOUSTICS;

BEAM; COMPOSITE; ELASTICITY; MATHEMATICAL MODELING; ROTOR; SPINNING; STABILITY; VIBRATION;

ARTICLE; CALCULATION; ELASTICITY; MATHEMATICAL MODEL; PRIORITY JOURNAL; ROTATION; SHEAR STRESS; VIBRATION;

EID: 0034896850     PISSN: 00014966     EISSN: None     Source Type: Journal    
DOI: 10.1121/1.1377292     Document Type: Article

References (11)

1. Anisotropy and structural coupling on vibration and instability of spinning thin-walled beams
2. Modeling and vibration of pretwisted spinning composite thin-walled beams
3. Dynamics of gyroelastic spacecraft
4. Stability of gyroelastic beams
5. The stability of a flexible link with a tip rotor and a compressive tip load
6. Free vibration of anisotropic composite thin-walled beams of closed cross-section contour
7. Refined structural modeling for enhancing vibrational and aeroelastic characteristics of composite aircraft wings
8. Vibration and stability of gyroelastic beams via smart materials technology
9. Control of cantilever vibration via structural tailoring and adaptive materials