Author:
Lemanski Stuart,Weaver Paul
Publisher
American Institute of Aeronautics and Astronautics
Reference6 articles.
1. Lemanski, S.L., Weaver, P.M., Hill, G.F.J. "Design of Composite Cylindrical Shells to meet given Cross Sectional Stiffness Properties" Proc, 43rdAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, andMaterials Conference,Denver,2002.
2. Miki, M., Sugiyama, Y. "Optimum Design of Laminated Composite Plates Using Lamination Parameters," Proc. AIAA/ASME/ASCE/AHS/ASC 32ndStructures, Structural Dynamics and Materials Conf, Baltimore, MA., Part I, pp.275-283,1991.
3. Kameyama, M., Fukunaga, H., Sekine, H. "Optimum Design of Composite Wing Model for Aeroelastic Properties," Proc.5thJapanIntl.SAMPESymposium,1997.
4. Stiffness design method of symmetric laminates using lamination parameters
5. A Laminate Design for Elastic Properties of Symmetric Laminates with Extension-Shear or Bending-Twisting Coupling