sample of publications

• articles 

  • Automatic testbed with a visual motion tracking system for airborne wind energy applications.  WIND ENERGY.  1-14. 2023
  • Three-dimensional unsteady aerodynamic analysis of a rigid-framed delta kite applied to airborne wind energy.  Energies.  14:1-17. 2021
  • Aerostructural wing shape optimization assisted by algorithmic differentiation..  STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION.  64:739-760. 2021
  • On the dynamic fluid-structure stability response of an innovative airplane configuration.  JOURNAL OF FLUIDS AND STRUCTURES.  105:1-20. 2021
  • Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis.  EUROPEAN JOURNAL OF CONTROL.  54:49-63. 2020
  • Nonlinear structural, nonlinear aerodynamic model for static aeroelastic problems.  AIAA JOURNAL.  57:2158-2170. 2019
  • Minimum Induced Drag Conditions for Truss-Braced Wings.  AIAA JOURNAL.  56. 2018
  • A Hybrid Reduced-Order Model for the Aeroelastic Analysis of Flexible Subsonic Wings: A Parametric Assessment.  Aerospace.  5:1-23. 2018
  • Equivalent Single Layer, Zig-Zag, and Layer Wise theories for variable angle tow composites based on the Generalized Unified Formulation.  Composite structures.  177:54-79. 2017
  • Minimum Induced Drag Theorems for Multiwing Systems.  AIAA JOURNAL.  55:3266-3287. 2017
  • Reduced basis methods for structurally nonlinear Joined Wings.  Aerospace Science and Technology.  68:486-495. 2017
  • Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future.  PROGRESS IN AEROSPACE SCIENCES.  87:1-93. 2016
  • Minimum induced drag theorems for joined wings, closed systems, and generic biwings: applications.  JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS.  169:236-261. 2016
  • Generalized Unified Formulation shell element for functionally graded Variable-Stiffness Composite Laminates and aeroelastic applications.  Composite structures.  131:501-515. 2015
  • Invariant Formulation for the Minimum Induced Drag Conditions of Nonplanar Wing Systems.  AIAA JOURNAL.  52:2223-2240. 2014
  • Nonlinear Analysis of PrandtlPlane Joined Wings: Effects of Anisotropy.  AIAA JOURNAL.  52:964-980. 2014

• book chapters 

  • Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings. In: Variational Analysis and Aerospace Engineering : Mathematical Challenges for the Aerospace of the Future.  SPRINGER CUSTOMER SERVICE CENTER GMBH. 191-217. 2016

• conference contributions 

  • A symbolic LFT approach for robust flutter analysis of high-order models.  961-967. 2019
  • A historical perspective on the aeroelasticity of Box Wings and PrandtlPlane with new findings.  0238 (1)-0238 (23). 2017
  • Zig-zag layerwise models for variable-stiffness composite laminates based on the generalized unified formulation.  0891 (1)-0891 (34). 2017
  • Geometrically non-linear structural modal model for aeroelastic applications.  1797 (1)-1797 (25). 2016
  • Minimum Induced Drag Theorems for Multi-Wing Systems.  0236 (1)-0236 (44). 2016
  • Nonlinear structural modal model for aeroelastic applications 2016