Aeroelastic airfoil smart spar

Composites Manufacturing - Tập 4 - Trang 195-198 - 1993
Skott Greenhalgh1, Christopher Pastore2, Moishe Garfinkle2
1Department of Textile Engineering, Chemistry, and Science, North Carolina State University, Raleigh, NC 27695, USA
2Department of Materials Engineering, Drexel University, Philadelphia, PA 19104, USA

Tài liệu tham khảo

Shirk, 1982, On the track of practical forward-swept wings, J Astronautics and Aeronautics Weisshaar, 1980, Divergence of forward swept composite wings, J Aircraft, 17, 442, 10.2514/3.57922 Smith, 1989, Formulation and evaluation of an analytical model for composite box-beams Chandra, 1990, Thin-walled composite beams under bending, torsional, and extensional loads, J Aircraft, 10.2514/3.25331 Chang-Ho, 1985, Aeroelastic stability analysis of a composite rotor blade, J American Helicopter Society, 57 Smith, 1989, Formulation and evaluation of an analytical model for composite box-beams Shirk, 1984, Aeroelastic tailoring-theory, practice and promise, J Aircraft, 23, 6, 10.2514/3.45260 Atanasoff, 1989, A manufacturing process for open mold mechanically coupled composite box beams with foam tooling, 798 Stemple, 1989, Large deflection static and dynamic finite element analysis of composite beams with arbitrary cross-sectional warping, 1788 Greenhalgh, 1992, Mechanical characterization of twisting-bending coupling on composite box-beam structures