ASD Lab

Publications

2020

  • Iannelli, A.Marcos, R.Bombardieri, R.Cavallaro, Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis, European Journal of Control, July 2020.

2019

  • Kantor, D.Raveh, R.Cavallaro, Nonlinear Structural, Nonlinear Aerodynamic Model for Static Aeroelastic Problems, AIAA Journal, February 2019.
  • Pustina, R.Cavallaro, G.Bernardini, NERONE: An Open-Source Based Tool for Aerodynamic Transonic Optimization of Nonplanar Wings, Aerotecnica Missili & Spazio, February 2019.

2018

  • Demasi, G.Monegato, R.Cavallaro, R.Rybarczyk, Minimum Induced Drag Conditions for Truss-Braced Wings, AIAA Journal, Vol.56, December 2018.
  • Berci, R.Cavallaro, A Hybrid Reduced-Order Model for the Aeroelastic Analysis of Flexible Subsonic Wings: A Parametric Assessment, Aerospace, Vol.76, July 2018.

2017

  • Andrea Cini; Philip Irving. Development of fatigue cracks from mechanically machined scratches on 2024-T351 aluminium alloy-Part I: experimentation and fractography analysis. Fatigue and Fracture of Engineering Material and Structures. 40 – 5, pp. 776 – 789. Wiley, 2017.
  • Philip Irving; Andrea Cini. Development of fatigue cracks from mechanically machined scratches on 2024-T351 aluminium alloy-Part II: finite element analysis and prediction method. Fatigue and Fracture of Engineering Material and Structures. 40 – 6, pp. 853 – 868. Wiley, 2017.
  • Demasi, G.Monegato, R.Cavallaro, Minimum Induced Drag Theorems for Multi- Wing Systems, AIAA Journal, Vol.55, October 2017.
  • Teunisse, P.Tiso, L.Demasi, R.Cavallaro, Reduced basis methods for structurally nonlinear Joined Wings, Journal of Aerospace Engineering, Vol.68, September 2017.
  • Demasi, G.Biagini, F.Vannucci, E.Santarpia, R.Cavallaro, Equivalent Single Layer, Zig-Zag, and Layer Wise Theories for Variable Angle Tow Composites Based on the Generalized Unified Formulation, Composite Structures, Vol.177, October 2017.

2016

  • Demasi, R.E.Gordnier, E.Santarpia, A.Dipace, R.Cavallaro, Aerodynamic and Structural Studies of a Flapping Wing in Forward Flight, AIAA Journal, Vol.54, No.9. 2016.
  • Cavallaro, L.Demasi, Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future, Invited: Progress in Aerospace Sciences, Vol.87, 2016.
  • Demasi, G.Monegato, A.DiPace, R.Cavallaro, Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory, Journal of Optimization Theory and Applications, Vol.169, No.1. 2016.
  • Demasi, G.Monegato, E.Rizzo, R.Cavallaro, A.DiPace., Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Results, Journal of Optimization Theory and Applications, Vol.169, No.1. 2016.

2015

  • Cavallaro, R.Bombardieri, A.Demasi, A.Iannelli., PrandtlPlane Joined Wing: Body Freedom Flutter, Limit Cycle Oscillation and Freeplay Studies, Journal of Fluids and Structures, Vol.59, November 2015.
  • Cavallaro, A.Iannelli, L.Demasi, A.M.Razon, Phenomenology of Nonlinear Aeroelastic Responses of Highly Deformable Joined Wings, Advances in Aircraft and Spacecraft Science, An International Journal, Vol.2, No.2. 2015.
  • Demasi, R.Cavallaro, Y.Ashenafi, E.Santarpia., Generalized Unified Formulation Shell Element for Functionally Graded Variable-Stiffness Composite Laminates and Aeroelastic Applications, Composite Structures, 2015.
  • Demasi, R.Cavallaro, F.Bertuccelli, Post-critical Analysis of Joined Wings: the Concept of Snap-Divergence as a Characterization of the Instability, Journal of Fluids and Structures, Vol.54, April 2015.

2014

  • Cavallaro, L.Demasi, F.Bertuccelli, D.J.Benson, Risks of Linear Design of Joined Wings: a Nonlinear Dynamic Perspective in the Presence of Follower Forces, CEAS Aeronautical Journal, November 2014.
  • Demasi, G.Monegato, A.Dipace, R.Cavallaro, Invariant Formulation for the Minimum Induced Drag Conditions of Non-planar Wing Systems, AIAA Journal, Vol.52, No.10. 2014.
  • Cavallaro, L.Demasi, A.Passariello, Nonlinear Analysis of PrandtlPlane Joined Wings: Effects of Anisotropy, AIAA Journal, Vol.52, No.5. 2014.

2013

  • Demasi, R.Cavallaro, A.M. Razon, Post-critical Analysis of PrandtlPlane Joined- Wing Configurations, AIAA Journal, Vol.51, No.1. 2013.

2012

  •  M Dorman; Nial Smith; Andrea Cini; Micheal Fitzpatrick; Philip Irving. Effect of laser shock peening on residual stress and fatigue life of clad 2024 aluminium sheet containing scribe defect. Material Science and Engineering A. 548, pp. 853 – 868. Elsevier, 2012.
  • Demasi, A.N.Palazotto, A.Hollenbeck, R.Cavallaro, Exploratory Structural Investigation of a Hawkmoth-Inspired MAV’s, International Journal of Micro Air Vehicles, Vol.4, No.4. 2012.

2010

  • Andrea Cini; Philip Irving. Transformation of defect into fatigue cracks; the role of Kt and defect scale on fatigue life of non-pristine components. Procedia Engineering. 2 – 1, pp. 667 – 677. Elsevier, 2010.

2009

  • YX Zhao; Philip Irving; Andrea Cini. Effect of laser shock peening on residual stress and fatigue life of clad 2024 aluminium sheet containing scribe defect. Material Science and Engineering A. 500 – 1-2, pp. 16 – 24. Elsevier, 2009.
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