San Diego State University

List of Publications (Luciano Demasi)




   Citation Indices (GOOGLE Scholar, Author ID: Luciano Demasi)


    Citations: 1453 (999 since 2012)

    h-index: 19 (16 since 2012)

    i10-index: 39 (33 since 2012)


   Citation Indices (SCOPUS, Author ID: 8637399400)


    Citations: 1390

    h-index: 18


   JOURNAL PAPERS


  1. L. Demasi, G. Monegato, R. Cavallaro, “Minimum Induced Drag Theorems for Multiwing Systems”, AIAA Journal, accepted (available in the a “article in advance” section), to appear in 2018


  2. P. Junghanns, G. Monegato,L. Demasi, “Properties and numerical solution of an integral equation to minimize airplane drag”, Festschrift for the 80th Birthday of Ian Sloan (Josef Dick, Frances Y Kuo, Henryk Wozniakowski, eds.), Springer-Verlag Heidelberg-Berlin, to appear in 2018


  3. L. Demasi, G. Biagini, F. Vannucci, E. Santarpia, R. Cavallaro, “Equivalent Single Layer, Zig-Zag and Layerwise Theories for Variable Angle Tow Composite Based on the Generalized Unified Formulation”, Composite Structures, Vol. 177, pp. 54-79, DOI: 10.1016/j.compstruct.2017.06.033, 2017


  4. N. Teunisse, P. Tiso, L. Demasi, R. Cavallaro, “Reduced Basis Methods for Structurally Nonlinear Joined Wings”, Aerospace Science and Technology, Vol. 68, pp-486-495, DOI: 10.1016/j.ast.2017.05.041, 2017


  5. L. 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, 1, pp-200-235, DOI: 10.1007/s10957-015-0849-y 2016


  6. L. Demasi, G. Monegato, E. Rizzo, R. Cavallaro A. Dipace, “Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Applications”, Journal of Optimization Theory and Applications, Vol. 169, 1, pp-236-261, DOI: 10.1007/s10957-015-0850-5 2016


  7. R. Cavallaro, L. Demasi, “Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future”, Progress in Aerospace Sciences, Vol. 87, pp. 1-93, DOI: 10.1016/j.paerosci.2016.07.002 2016


  8. L. Demasi, E. Santarpia, A. Dipace, R. Cavallaro, R. E. Gordnier, “Aerodynamic and Structural Studies of a Flapping Wing in Forward Flight”, AIAA Journal, Vol. 54, 9, pp-2768-81, DOI: 10.2514/1.J054496 2016


  9. R. Cavallaro, R. Bombardieri, L. Demasi, A. Iannelli, “PrandtlPlane Joined Wing: Body Freedom Flutter, Limit Cycle Oscillation and Freeplay Studies”, AIAA Journal, Vol. 51, No. 1: pp 161-177, Journal of Fluids and Structures, Vol. 59, No. 11, pp. 57-84, DOI: 10.1016/j.jfluidstructs.2015.08.016 2015


  10. L. Demasi, Y. Ashenafi, R. Cavallaro, E. Santarpia, “Generalized Unified Formulation Shell Element for Variable-Stiffness Composite Laminates and Aeroelastic Applications”, Composite Structures, Vol. 131, pp. 501-515, DOI: 10.1016/j.compstruct.2015.05.022 2015


  11. R. Cavallaro, A. Iannelli, L. Demasi, and A. M. Razσn, “Phenomenology of Nonlinear Aeroelastic Responses of Highly Deformable Joined Wings”, Advances in Aircraft and Spacecraft Science, Vol. 2, No. 2, pp. 125-168, 2015


  12. L. Demasi, R. Cavallaro, and 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, pp. 701-718, DOI: 10.1016/j.jfluidstructs.2015.01.009 2015


  13. R. Cavallaro, L. Demasi, F. Bertuccelli, D. Benson , “Risks of Linear Design of Joined Wings: a Nonlinear Dynamic Perspective in the Presence of Follower Forces”, CEAS Aeronautical Journal, Vol. 6, No. 2, pp. 161-180, DOI 10.1007/s13272-014-0136-x 2015


  14. L. Demasi, A. Dipace, G. Monegato, and R. Cavallaro, “An Invariant Formulation for the Minimum Induced Drag Conditions of Non-planar Wing systems”, AIAA Journal, Vol. 52, No. 10, pp. 2223-2240, 2014, DOI: 10.2514/1.J052837, 2014


  15. R. Cavallaro, L. Demasi, A. Passariello, “Nonlinear Analysis of PrandtlPlane Joined Wings: Effects of Anisotropy”, AIAA Journal, Vol. 52, No. 5, pp. 964-980, 2014


  16. L. Demasi, R. Cavallaro, and A. M. Razσn, “Post-Critical Analysis of PrandtlPlane Joined-Wing Configurations”, AIAA Journal, Vol. 51, No. 1: pp 161-177, DOI: 10.2514/1.J051700, 2013


  17. E. Carrera, A. Varello, L. Demasi, “A Refined Structural Model for Static Aeroelastic Response and Divergence of Metallic and Composite Wings”, CEAS Aeronautical Journal, Vol. 4, No. 2, pp 175-189, 2013.


  18. L. Demasi, “ Partially Layer Wise Advanced Zig Zag and HSDT Models Based on the Generalized Unified Formulation”, Engineering Structures, Vol. 53, pp 63-91, 2013.


  19. L. Demasi, W. Yu, “ Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis Using the Generalized Unified Formulation”, Mechanics of Advanced Materials and Structures, Vol. 20, No. 3, pp 227-241, 2013.


  20. L. Demasi, A. N. Palazotto, A. Hollenbeck, R. Cavallaro, “Exploratory Structural Investigation of a Hawkmoth-Inspired MAV’s Thorax”, International Journal of Micro Air Vehicles, Vol. 4, No. 4, 2012.


  21. L. Demasi, “Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation”, Composite Structures, Vol. 94 (2), pg. 363-375, 2012.


  22. E. Carrera, F. A. Fazzolari, and L. Demasi, “Vibration Analysis of Anisotropic Simply Supported Plates by using Variable Kinematic and Rayleigh-Ritz Method”, Journal of Vibration and Acoustics, Vol. 133, pp. 1-18, 2011.


  23. A. Varello, E. Carrera, L. Demasi, “ Vortex Lattice Method Coupled with Advanced One-Dimensional Structural Models”, ASD Journal, Vol. 2, pp. 53-78, 2011.


  24. A. V. Styuart, E. Livne, L. Demasi, M. Mor, “Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures”, AIAA Journal, vol. 49, 655-669, 2011.


  25. L. Demasi, “An Invariant Finite Element Model for Composite Structures: the Generalized Unified Formulation”, AIAA Journal, Vol. 48, No. 8, 2010.


  26. L. Demasi, “Three-dimensional closed form solutions and ∞3 theories for orthotropic plates”, Mechanics of Advanced Materials and Structures, Vol. 17, 20-39, 2010.


  27. S. Brischetto, E. Carrera, L. Demasi, “Improved Bending Analysis of sandwich plates using Zig-Zag function”, Composite structures, Vol. 89, 408-415, 2009.


  28. S. Brischetto, E. Carrera, L. Demasi, “Improved response of unsymmetrically laminated Sandwich Plates by using Zig-Zag functions”, Journal of Sandwich Structures and Materials, Vol. 11, 257-267, 2009.


  29. S. Brischetto, E. Carrera, L. Demasi, “Free vibration of sandwich plates and shells by using Zig-Zag function”, Shock and Vibration, 16, 495-503, 2009.


  30. L. Demasi, E. Livne, “Aeroelastic coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics – Two Formulations”, Journal of Fluids and Structures, Vol. 25, 918-935, 2009.


  31. L. Demasi, E. Livne, “ Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces”, AIAA Journal, Vol. 47, No. 1, 2009.


  32. L. Demasi, “6 mixed plate theories based on the Generalized Unified Formulation. Part I: Governing Equations” Composite Structures, Vol. 87, (2009), 1-11.


  33. L. Demasi, “6 mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories” Composite Structures, Vol. 87, (2009), 12-22.


  34. L. Demasi, “6 mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced Mixed High Order Shear Deformation Theories” Composite Structures, Vol. 87, (2009), 183-194.


  35. L. Demasi, “6 mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-Zag Theories” Composite Structures, Vol. 87, (2009), 195-205.


  36. L. Demasi, “6 mixed plate theories based on the Generalized Unified Formulation. Part V: Results” Composite Structures, Composite Structures, Vol. 88, (2009), 1-16.


  37. L. Demasi, “2D, Quasi 3D and 3D Exact Solutions for Bending of Thick and Thin Sandwich Plates”, Journal of Sandwich Structures & Materials, Vol. 10, No. 4, 271-310, DOI: 10.1177/1099636208089311, 2008.


  38. L. Demasi, “3 plate theories for thick and thin plates: the generalized unified formulation”, Composite Structures, 84 (2008) 256-270


  39. L. Demasi, “Three-Dimensional Closed Form Solutions and Exact Thin Plate Theories for Isotropic Plates”, Composite Structures 2007, 80, pp. 183-195, doi:10.1016/compstruct.2006.04.073


  40. L. Demasi, “A Theoretical Investigation on the Conditions of Minimum Induced Drag of Closed Wing Systems and C-Wings”, Journal of Aircraft, Vol. 44, No. 1, 2007, 81-99


  41. L. Demasi, “Treatment of Stress Variables in Advanced Multilayered Plate Elements Based Upon Reissner's Mixed Variational Theorem”, Computers & Structures 2006, 84, pp. 1215-1221


  42. L. Demasi, “Quasi-3D Analysis of Free Vibration of Anisotropic Plates”, Composite Structures 2006, 74, pp. 449-457.


  43. L. Demasi, “Induced Drag Minimization: a Variational Approach Using the Acceleration Potential”, Journal of Aircraft, Vol.43, No. 3, 2006, pp. 669-680


  44. L. Demasi, E. Livne, “Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach - An Assessment”, Journal of Aircraft Vol. 43, No. 6, 2006, pp. 1685-1697


  45. L. Demasi, “Refined Multilayered Plate Elements Based on Murakami Zig-Zag Functions”, Composite Structures 2005, 70, pp. 308-316.


  46. E. Carrera, L. Demasi, “Two benchmarks to assess two-dimensional theories of Sandwich Composite Plates”, AIAA Journal Vol. 41, No. 7, pp. 1356-1362, July 2003.


  47. E. Carrera, L. Demasi, M. Manganello, “An Assessment of Plate Elements on Bending and Vibrations of Composite Structures”, Mechanics of Composite Material and Structures, 9:333-357, 2002.


  48. E. Carrera, L. Demasi, “Classical and advanced Multilayered plate element based upon PVD and RMVT. Part I : Derivation of finite element matrices” International Journal for Numerical Methods in Engineering 2002; 55: 191-231.


  49. E. Carrera, L. Demasi, “Classical and advanced Multilayered plate element based upon PVD and RMVT. Part II: Numerical implementations” International Journal for Numerical Methods in Engineering 2002; 55: 253-291.

   BOOKS


  1. E. Carrera, L. Demasi, “Appunti di Costruzioni Aeronautiche A” (English translation of the title: “Notes of Aeronautical Constructions A”) Levrotto & Bella, Torino, 2002.

   Articles in Book


  1. L. Demasi, G. Monegato, R. Cavallaro, “Minimum Induced Drag Theorems for Nonplanar Systems and Closed Wings”, in A. Frediani (Ed.), Variational Analysis and Aerospace Engineering III: Mathematical Challenges for the Aerospace of the Future, Springer U.S., 2017


  2. R. Cavallaro, R. Bombardieri, S. Silvani, L. Demasi, and G. Bernardini, “Aeroelasticity of the PrandtlPlane: Body Freedom Flutter, Freeplay and Limit Cycle Oscillation”, in A. Frediani (Ed.), Variational Analysis and Aerospace Engineering III: Mathematical Challenges for the Aerospace of the Future, Springer U.S., 2017

   Conference Papers (Peer Reviewed)


  1. L. Demasi, G. Biagini, F. Vannucci, E. Santarpia, R. Cavallaro, “Equivalent Single Layer, Zig-Zag and Layerwise Theories for Variable Angle Tow Composite Based on the Generalized Unified Formulation”, AIAA Science and Technology Forum and Exposition: 58th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference 2017


  2. L. Demasi, G. Monegato, R. Cavallaro, “Minimum Induced Drag Theorems for Multi-Wing Systems”, AIAA Science and Technology Forum and Exposition: 57th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 2016


  3. R. Bombardieri, R. Cavallaro,L. Demasi, “A Historical Perspective on the Aeroelasticity of Box Wings and PrandtlPlane with New Findings”, AIAA Science and Technology Forum and Exposition: 57th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 2016


  4. L. Demasi, Y. Ashenafi, R. Cavallaro, E. Santarpia, “Generalized Unified Formulation Shell Element for Variable-Stiffness Composite Laminates and Aeroelastic Applications”, AIAA Science and Technology Forum and Exposition: 56th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 2015


  5. L. Demasi, G. Monegato, A. Dipace, R. Cavallaro, “Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings. Part I: Theory”, AIAA Science and Technology Forum and Exposition: 56th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 2015


  6. L. Demasi, G. Monegato, E. Rizzo, R. Cavallaro A. Dipace, “Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings. Part II: Results”, AIAA Science and Technology Forum and Exposition: 56th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 2015


  7. N. Teunisse, P. Tiso, L. Demasi, and R. Cavallaro, “Computational Reduced Order Methods for Structurally Nonlinear Joined Wings”, AIAA Science and Technology Forum and Exposition: 56th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 2015


  8. R. Cavallaro, M. Nardini, L. Demasi, “Amphibious PrandtlPlane: Preliminary Design Aspects Including Propeller's Integration and Ground Effect”, AIAA Science and Technology Forum and Exposition: 56th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 2015


  9. R. Cavallaro, L. Demasi, R. Bombardieri, and A. Iannelli, “PrandtlPlane Joined Wing: Body Freedom Flutter, Limit Cycle Oscillation and Freeplay Studies”, AIAA Science and Technology Forum and Exposition: 56th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference 2015


  10. G. Phlipot, X. Q. Wang, M. Mignolet, L. Demasi, R. Cavallaro, “Nonintrusive Reduced Order Modeling for the Nonlinear Geometric Response of Some Joined Wings”, AIAA Science and Technology Forum and Exposition: 55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, January 2014.


  11. G. N. Teunisse, L. Demasi, P. Tiso, R. Cavallaro, “A Computational Method for Structurally Nonlinear Joined Wings Based on Modal Derivatives”, AIAA Science and Technology Forum and Exposition: 55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, January 2014.


  12. R. Cavallaro, A. Iannelli, L. Demasi, A. M. Razσn, “Phenomenology of Nonlinear Aeroelastic Responses of Highly Deformable Joined-wings Configurations”, AIAA Science and Technology Forum and Exposition: 55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, January 2014.


  13. L. Demasi, A. Dipace, G. Monegato, and R. Cavallaro, “An Invariant Formulation for the Minimum Induced Drag Conditions of Non-planar Wing systems”, AIAA Science and Technology Forum and Exposition: 55th AIAA/ASME/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, January 2014.


  14. R. Gordnier and L. Demasi, “Implicit LES Simulations of Flapping Wing in Forward Flight”, ASME 2013 Fluids Engineering Summer Conference, Incline Village, Nevada, July 7-11, 2013.


  15. R. Cavallaro, L. Demasi, F. Bertuccelli, “Risks of Linear Design of Joined Wings: a Nonlinear Dynamic Perspective in the Presence of Follower Forces”, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Boston, Massachusetts, April 2013.


  16. L. Demasi, R. Cavallaro, F. Bertuccelli, “Post-Critical Analysis of Joined Wings: the Concept of Snap-Divergence as a Characterization of the Instability”, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Boston, Massachusetts, April 2013.


  17. L. Demasi, R. E. Gordnier, E. Santarpia, A. Dipace, “High-fidelity Simulations of a Flexible Flapping Wing in Forward flight”, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Boston, Massachusetts, April 2013.


  18. L. Demasi, A. N. Palazotto, A. Hollenbeck, R. Cavallaro, “Exploratory Structural Investigation of a Hawkmoth-Inspired MAV’s Thorax”, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Honolulu, Hawaii, April 2012.


  19. L. Demasi, “Partially Layerwise Advanced Zig-Zag and HSDT Models Based on the Generalized Unified Formulation”, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Honolulu, Hawaii, April 2012.


  20. S. Bhasin, P. C. Chen, Z., Wang, L. Demasi, “Dynamic Nonlinear Aeroelastic Analysis of The Joined Wing Configurationon”, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Honolulu, Hawaii, April 2012.


  21. R. Cavallaro, L. Demasi, A. Passariello, “Nonlinear Analysis of PrandtlPlane Joined Wings-Part II: Effects of Anisotropy”, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Honolulu, Hawaii, April 2012.


  22. L. Demasi, “Partially Zig-Zag Advanced Shear Deformation Theories Based on the Generalized Unified Formulation”, 16th International Conference on Composite Structures (ICCS16), Porto, Portugal, 28-30 June 2011.


  23. M. Petrolo, E. Carrera, L. Demasi, “An Advanced Unified Aeroelastic Formulation Based on 1D Higher-Order Finite Elements”, International Forum of Aeroelasticity and Structural Dynamics, Paris, France, 26-30 June 2011.


  24. L. Demasi, K. Hasslinger, and D. Samardzic, “Multi-Theory FEM Architecture for the Generation of Advanced Mixed Shear Deformation Theories Based on the Generalized Unified Formulation for Composite Structures”, 25th Annual Technical Conference (American Society for Composites), Dayton, OH, 20-22 September 2010.


  25. L. Demasi, A. Palacios, “A Reduced Order Nonlinear Aeroelastic Analysis of Joined Wings Based on the Proper Orthogonal Decomposition”, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Orlando, Florida, 12-15 April 2010.


  26. A. Varello, L. Demasi, E. Carrera, G. Giunta, “An Improved Beam Formulation for Aeroelastic Applications”, 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Orlando, Florida, 12-15 April 2010.


  27. L. Demasi, “An Invariant Model for any Composite Plate Theory and FEM Applications: the Generalized Unified Formulation”, 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Palm Springs, California, 4-7 May 2009.


  28. L. Demasi, W. Yu, “Assess the Accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) Using the Generalized Unified Formulation (GUF)”, 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Palm Springs, California, 4-7 May 2009.


  29. L. Demasi, E. Livne, “Contributions to Joined-Wing Aeroelasticity”, International Forum on Aeroelasticity and Structural Dynamics, Seattle, Washington, 21-25 June 2009.


  30. L. Demasi, E. Livne, “Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady Aerodynamics: Two Formulations”, 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Schaumburg, Illinois, 7-10 April 2008.


  31. L. Demasi, E. Livne, “Dynamic Aeroelasticity of Coupling Full Order Geometrically Nonlinear Structurs and Full Order Linear Unsteady Aerodynamic – The Joined Wing Case”, 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Schaumburg, Illinois, 7-10 April 2008.


  32. A. Styuart, L. Demasi, E. Livne and K. Lin, “Probabilistic Modeling of the Aeroelastic Life Cycle for Risk Evaluation of Composite Structures”, 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Schaumburg, Illinois, 7-10 April 2008.


  33. L. Demasi, E. Livne, “Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear Modally Reduced Aerodynamic Generalized Forces”, 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Honolulu, Hawaii, 23-26 April 2007.


  34. L. Demasi, E. Livne, “The Structural Order Reduction Challenge in the Case of Geometrically Nonlinear Joined-Wing Configurations”, 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Honolulu, Hawaii, 23-26 April 2007.


  35. L. Demasi, E. Livne, “Aeroelasticity of Structurally Nonlinear Lifting Surfaces Using Linear Modally Reduced Aerodynamic Generalized Forces”, 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Newport, Rhode Island, 1-4 May 2006.


  36. L. Demasi, E. Livne, “Exploratory Studies of Joined Wing Aeroelasticity”, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Austin, Texas, 18-21 April 2005.


  37. L. Demasi, E. Livne, “Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Approach – An Assessment”, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, Austin, Texas, 18-21 April 2005.


  38. L. Demasi, E. Livne, “A Plate Structural Capability for the Nonlinear Aeroelastic Analysis of Joined-Wing Configurations”, Italian Conference AIDAA Roma (Italy), 15-19th September 2003.


  39. L. Demasi, “Ala Anulare Ellittica: Distribuzione di Circolazione di Minima Resistenza Indotta” (English translation of the title: “Elliptical Annular Wing: Circulation of Minimum Induced Drag”), Italian Conference AIDAA Roma (Italy), 15-19th September 2003.


  40. L. Demasi, “Effetto delle condizioni al contorno sulla modellizzazione di piastre multistrato” (English translation of the title: “Effects of the Boundary Conditions for 2D Models of Multilayered Plates”), Italian Conference AIDAA Palermo (Italy), 24-28th September 2001.


  41. A. Robaldo, L. Demasi, E. Carrera, “Influence of Temperature Profile on the Accuracy of Classical and Refined Multilayered Plate” Italian Conference GIMC Genova (Italy), 21-23th June 2004.


  42. E. Carrera, L. Demasi, “On Two-Dimensional FEM Simulation of Layered Plates” GIMC Conference, Giulianova 24-26 June 2002 24-26 June, 2002.


  43. E. Carrera, L. Demasi, “Sandwich Plate Analysis by Finite Element Method and Reissner's Mixed Theorem” Fifth International Conference on Sandwich Construction Zurich (Switzerland), 5-7th September 2000.


  44. E. Carrera, L. Demasi, “An Assessment of Multilayered Finite Plate Elements in View of the C0z Requirements” Italian Conference GIMC 2000 Brescia (Italy), 13-15th November 2000.


  45. E. Carrera, G. Chiocchia, L. Demasi, A. Robaldo, “On the developments of a Joined Wing Prandtlplane” Fifth World Congress on Computational Mechanics,Vienna July 7-12 2002.


  46. L. Demasi, G. Chiocchia, E. Carrera, “Aerodinamica dei Sistemi Portanti Chiusi: Ala Anulare Ellittica” (English translation of the title: “Aerodynamics of the closed Wing Systems: Elliptical Annular Wing”) Italian Conference AIDAA Roma (Italy), 15-19th Sept. 2003.


  47. G. Chiocchia, E. Carrera, L. Demasi, “Studio Aerodinamico di un’Ala Anulare Ellittica” (English translation of the title: “Aerodynamic Studies of an Elliptical Annular Wing”) Italian Conference AIDAA Palermo (Italy), 24-28th September 2001.

   Other Publications (Alenia Spazio Internal Reports)


  1. L. Demasi et alii, “RADARSAT-2 Stress Summary Report, Issue 1, Date 25/11/2001” ALENIA SPAZIO Internal report, 2001


  2. L. Demasi et alii, “RADARSAT-2 Static Analysis Report, Issue 4, Date 22/11/2001” ALENIA SPAZIO Internal report, 2001