Dynamic behavior of aircraft wings modeled as doubly-tapered composite thin-walled beams

American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP

Volumn 398, Issue , 1999, Pages 59-68

  Na, Sungsoo ^a   Librescu, Liviu ^b  

^a Korea Polytechnic University   (South Korea)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEFORMATION; DYNAMIC RESPONSE; MATHEMATICAL MODELS; SHEAR STRESS; STRESS ANALYSIS; VIBRATIONS (MECHANICAL); WINGS;

THIN WALLED BEAMS; TRANSVERSE SHEAR; WARPING;

COMPOSITE BEAMS AND GIRDERS;

EID: 0033319901     PISSN: 0277027X     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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8. Librescu, L., Meirovitch, L. and Song, O., "Refined Structural Modeling for Enhancing Vibrational and Aeroelatic Characteristics of Composite Aircraft Wings," La Recherche Aerospatiale, 1, pp. 23-35, 1996.
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12. Downs, B., "Transverse Vibrations of Cantilever Beams Having Unequal Breadth and Dept. Tapers", Journal of Applied Mechanics, Trans. ASME, December 1977, pp. 737-742.