Optimal thickness distributions of aeroelastic flapping shells

[1]  Carlos E. S. Cesnik,et al.  Flapping-Wing Structural Dynamics Formulation Based on a Corotational Shell Finite Element , 2011 .

[2]  Bret Stanford,et al.  Formulation of Analytical Design Derivatives for Nonlinear Unsteady Aeroelasticity , 2010 .

[3]  Bret Stanford,et al.  Shape, Structure, and Kinematic Parameterization of a Power-Optimal Hovering Wing , 2010 .

[4]  Hu Dai,et al.  A 3D computational study of the flow-structure interaction i n flapping flight , 2010 .

[5]  Scott L. Thomson,et al.  Shape Optimization and Fluid Dynamic Analysis of a Translating Flexible Body , 2010 .

[6]  John Young,et al.  Details of Insect Wing Design and Deformation Enhance Aerodynamic Function and Flight Efficiency , 2009, Science.

[7]  Bret Stanford,et al.  Analytical Sensitivity Analysis of an Unsteady Vortex Lattice Method for Flapping Wing Optimization , 2009 .

[8]  Wright-Patterson Afb,et al.  Cost Reduction Techniques for the Structural Design of Nonlinear Flapping Wings , 2009 .

[9]  Carlos E. S. Cesnik,et al.  Flapping Wing CFD/CSD Aeroelastic Formulation Based on a Co- rotational Shell Finite Element , 2009 .

[10]  Inderjit Chopra,et al.  Insect-Based Hover-Capable Flapping Wings for Micro Air Vehicles: Experiments and Analysis , 2008 .

[11]  Koji Isogai,et al.  Optimum Aeroelastic Design of a Flapping Wing , 2007 .

[12]  Qiang Zhu,et al.  Numerical Simulation of a Flapping Foil with Chordwise or Spanwise Flexibility , 2007 .

[13]  Masaki Hamamoto,et al.  Application of fluid–structure interaction analysis to flapping flight of insects with deformable wings , 2007, Adv. Robotics.

[14]  Tanakorn Tantanawat,et al.  Design of Compliant Mechanisms for Minimizing Input Power in Dynamic Applications , 2007 .

[15]  Sam Heathcote,et al.  Effect of Spanwise Flexibility on Flapping Wing Propulsion , 2006 .

[16]  M. Platzer,et al.  Flapping Wing Aerodynamics - Progress and Challenges , 2006 .

[17]  J. Alonso,et al.  A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design , 2005 .

[18]  Lyle N. Long,et al.  Object-oriented unsteady vortex lattice method for flapping flight , 2004 .

[19]  Chih-Ming Ho,et al.  Unsteady aerodynamics and flow control for flapping wing flyers , 2003 .

[20]  Tamer M. Wasfy,et al.  Computational strategies for flexible multibody systems , 2003 .

[21]  T. Daniel,et al.  Into thin air: contributions of aerodynamic and inertial-elastic forces to wing bending in the hawkmoth Manduca sexta , 2003, Journal of Experimental Biology.

[22]  T. Daniel,et al.  The Journal of Experimental Biology 206, 2989-2997 © 2003 The Company of Biologists Ltd , 2003 .

[23]  Kyung K. Choi,et al.  DESIGN SENSITIVITY ANALYSIS AND OPTIMIZATION OF NONLINEAR TRANSIENT DYNAMICS* , 2000 .

[24]  H. Yoo,et al.  DYNAMICS OF RECTANGULAR PLATES UNDERGOING PRESCRIBED OVERALL MOTION , 2001 .

[25]  M. Crisfield,et al.  Energy‐conserving and decaying Algorithms in non‐linear structural dynamics , 1999 .

[26]  E. Madenci,et al.  DYNAMIC RESPONSE OF THIN COMPOSITE SHELLS EXPERIENCING NON-LINEAR ELASTIC DEFORMATIONS COUPLED WITH LARGE AND RAPID OVERALL MOTIONS , 1996 .

[27]  M. Dickinson.  Directional Sensitivity and Mechanical Coupling Dynamics of Campaniform Sensilla During Chordwise Deformations of the Fly Wing , 1992 .

[28]  K. Svanberg.  The method of moving asymptotes—a new method for structural optimization , 1987 .

[29]  R. Haftka,et al.  Elements of Structural Optimization , 1984 .

[30]  R. Cook,et al.  Concepts and Applications of Finite Element Analysis , 1974 .