The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations
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[1] Pma Paul Slaats,et al. MODEL REDUCTION TOOLS FOR NONLINEAR STRUCTURAL DYNAMICS , 1995 .
[2] Alberto Cardona,et al. A reduction method for nonlinear structural dynamic analysis , 1985 .
[3] Luciano Demasi,et al. Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces , 2006 .
[4] D. Shalev,et al. Nonlinear analysis using a modal-based reduction technique , 1995 .
[5] Luciano Demasi,et al. Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces , 2007 .
[6] Eli Livne,et al. Future of Airplane Aeroelasticity , 2003 .
[7] Terrence A. Weisshaar,et al. Aeroelasticity of Nonconventional Airplane Configurations-Past and Future , 2003 .
[8] J. Giesing,et al. Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic Flow , 1970 .
[9] Eli Livne,et al. Structural Dynamic Frequency Response Using Combined Direct and Adjoint Reduced-Order Approximations , 2003 .
[10] Mordehai Karpel,et al. Stress Considerations in Reduced-Size Aeroelastic Optimization , 1995 .
[11] N. F. Knight,et al. Nonlinear structural dynamic analysis using a modified modal method , 1985 .
[12] M. Karpel,et al. Efficient vibration mode analysis of aircraft with multiple external store configurations , 1988 .
[13] Robert Levy,et al. Triangular Shell Element for Large Rotations Analysis , 2003 .
[14] Earl H. Dowell,et al. Modeling the LCO of a Delta Wing Using a High , 2004 .
[15] Eli Livne,et al. Reduced-order design-oriented stress analysis using combined direct and adjoint solutions , 2000 .
[16] Robert Levy,et al. The geometric stiffness of triangular composite-materials shell elements , 2005 .
[17] Mordechay Karpel,et al. Modal-Based Enhancement of Integrated Design Optimization Schemes , 1998 .
[18] Erwin Sulaeman,et al. Effect of Compressive Force on Aeroelastic Stability of a Strut-Braced Wing , 2001 .
[19] J. Katz,et al. Low-Speed Aerodynamics , 1991 .
[20] William P. Rodden,et al. Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic Flow , 1971 .
[21] Luciano Demasi,et al. Exploratory Studies of Joined Wing Aeroelasticity , 2005 .
[22] Earl H. Dowell,et al. Modeling delta wing limit-cycle oscillations using a high-fidelity structural model , 2005 .
[23] Paolo Tiso,et al. A Finite Element Based Reduction Method for Nonlinear Dynamics of Structures , 2005 .
[24] William P. Rodden,et al. Further Refinement of the Subsonic Doublet-Lattice Method , 1998 .