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Luciano Demasi - Publications

Affiliations: 
Structural Engineering San Diego State University, San Diego, CA, United States 
Area:
Civil Engineering
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63 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2020 Russo L, Tognaccini R, Demasi L. Box Wing and Induced Drag: Compressibility Effects in Subsonic and Transonic Regimes Aiaa Journal. 58: 2398-2413. DOI: 10.2514/1.J059080  0.311
2020 Santarpia E, Demasi L. Large displacement models for composites based on Murakami's Zig-Zag Function, Green-Lagrange Strain Tensor, and Generalized Unified Formulation Thin-Walled Structures. 150: 106460. DOI: 10.1016/J.Tws.2019.106460  0.441
2017 Demasi L, Biagini G, Vannucci F, Santarpia E, Cavallaro R. 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. DOI: 10.1016/J.Compstruct.2017.06.033  0.523
2017 Teunisse N, Demasi L, Tiso P, Cavallaro R. Reduced basis methods for structurally nonlinear Joined Wings Aerospace Science and Technology. 68: 486-495. DOI: 10.1016/J.Ast.2017.05.041  0.415
2016 Demasi L, Monegato G, Cavallaro R. Minimum Induced Drag Theorems for Multi-Wing Systems Aiaa Journal. 55: 3266-3287. DOI: 10.2514/1.J055652  0.326
2016 Demasi L, Santarpia E, Dipace A, Cavallaro R, Gordnier RE. Aerodynamic and structural studies of a flapping wing in forward flight Aiaa Journal. 54: 2768-2781. DOI: 10.2514/1.J054496  0.331
2016 Cavallaro R, Demasi L. 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. DOI: 10.1016/J.Paerosci.2016.07.002  0.38
2016 Demasi L, Monegato G, Rizzo E, Cavallaro R, Dipace A. Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Applications Journal of Optimization Theory and Applications. 169: 236-261. DOI: 10.1007/S10957-015-0850-5  0.432
2016 Demasi L, Monegato G, Dipace A, Cavallaro R. Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory Journal of Optimization Theory and Applications. 169: 200-235. DOI: 10.1007/S10957-015-0849-Y  0.424
2015 Cavallaro R, Bombardieri R, Demasi L, Iannelli A. PrandtlPlane Joined Wing: Body freedom flutter, limit cycle oscillation and freeplay studies Journal of Fluids and Structures. 59: 57-84. DOI: 10.1016/J.Jfluidstructs.2015.08.016  0.353
2015 Demasi L, Cavallaro R, Bertuccelli F. Post-critical analysis of highly deformable Joined Wings: The concept of snap-divergence as a characterization of the instability Journal of Fluids and Structures. 54: 701-718. DOI: 10.1016/J.Jfluidstructs.2015.01.009  0.407
2015 Demasi L, Ashenafi Y, Cavallaro R, Santarpia E. Generalized Unified Formulation shell element for functionally graded Variable-Stiffness Composite Laminates and aeroelastic applications Composite Structures. 131: 501-515. DOI: 10.1016/J.Compstruct.2015.05.022  0.516
2015 Cavallaro R, Demasi L, Bertuccelli F, Benson DJ. Risks of linear design of joined wings: a non-linear dynamic perspective in the presence of follower forces Ceas Aeronautical Journal. 6: 161-180. DOI: 10.1007/S13272-014-0136-X  0.376
2014 Cavallaro R, Iannelliy A, Demasi L, Razón AM. Phenomenology of nonlinear aeroelastic responses of highly deformable joined-wings configurations 55th Aiaa/Asme/Asce/Ahs/Sc Structures, Structural Dynamics, and Materials Conference. DOI: 10.2514/6.2014-1199  0.325
2014 Demasi L, Dipace A, Monegatom G, Cavallaro R. Invariant formulation for the minimum induced drag conditions of nonplanar wing systems Aiaa Journal. 52: 2223-2240. DOI: 10.2514/1.J052837  0.415
2014 Cavallaro R, Demasi L, Passariello A. Nonlinear analysis of prandtlplane joined wings: Effects of anisotropy Aiaa Journal. 52: 964-980. DOI: 10.2514/1.J052242  0.398
2013 Demasi L, Cavallaro R, Bertuccelli F. Post-critical analysis of joined wings: The concept of snap-divergence as a characterization of the instability Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/6.2013-1559  0.314
2013 Demasi L, Cavallaro R, Razón AM. Postcritical analysis of prandtlplane joined-wing configurations Aiaa Journal. 51: 161-177. DOI: 10.2514/1.J051700  0.387
2013 Demasi L, Yu W. Assess the accuracy of the variational asymptotic plate and shell analysis using the generalized unified formulation Mechanics of Advanced Materials and Structures. 20: 227-241. DOI: 10.1080/15376494.2011.584150  0.316
2013 Demasi L. Partially layer wise advanced zig zag and HSDT models based on the generalized unified formulation Engineering Structures. 53: 63-91. DOI: 10.1016/J.Engstruct.2013.01.021  0.494
2013 Carrera E, Varello A, Demasi L. A refined structural model for static aeroelastic response and divergence of metallic and composite wings Ceas Aeronautical Journal. 4: 175-189. DOI: 10.1007/S13272-013-0063-2  0.443
2012 Demasi L, Palazotto A, Hollenbeck A, Cavallaro R. Exploratory structural investigation of a hawkmoth-inspired MAV's thorax International Journal of Micro Air Vehicles. 4: 291-304. DOI: 10.1260/1756-8293.4.4.291  0.347
2012 Demasi L. Partially Zig-Zag Advanced Higher Order Shear Deformation Theories Based on the Generalized Unified Formulation Composite Structures. 94: 363-375. DOI: 10.1016/J.Compstruct.2011.07.022  0.484
2012 Demasi L. Partially layer-wise advanced zig-zag and HSDT models based on the generalized unified formulation Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.422
2012 Demasi L. Partially layer-wise advanced zig-zag and HSDT models based on the generalized unified formulation Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.422
2011 Styuart AV, Livne E, Demasi L, Mor M. Flutter failure risk assessment for damage-tolerant composite aircraft structures Aiaa Journal. 49: 655-669. DOI: 10.2514/1.J050862  0.31
2011 Carrera E, Fazzolari FA, Demasi L. Vibration analysis of anisotropic simply supported plates by using variable kinematic and rayleigh-ritz method Journal of Vibration and Acoustics, Transactions of the Asme. 133. DOI: 10.1115/1.4004680  0.472
2010 Demasi L. Invariant finite element model for composite structures: The generalized unified formulation Aiaa Journal. 48: 1602-1619. DOI: 10.2514/1.45416  0.541
2010 Demasi L. Three-dimensional closed form solutions and 3 theories for orthotropic plates Mechanics of Advanced Materials and Structures. 17: 20-39. DOI: 10.1080/15376490802665684  0.534
2010 Demasi L, Palacios A. A reduced order nonlinear aeroelastic analysis of Joined Wings based on the Proper Orthogonal Decomposition Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.32
2010 Varello A, Demasi L, Carrera E, Giunta G. An improved beam formulation for aeroelastic applications Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.353
2010 Demasi L, Hasslinger K, Samardzic D. Multi-theory FEM architecture for the generation of advanced mixed shear deformation theories based on the Generalized Unified Formulation for composite structures 25th Technical Conference of the American Society For Composites and 14th Us-Japan Conference On Composite Materials 2010. 2: 1491-1511.  0.424
2009 Brischetto S, Carrera E, Demasi L. Free vibration of sandwich plates and shells by using zig-zag function Shock and Vibration. 16: 495-503. DOI: 10.3233/Sav-2009-0483  0.432
2009 Brischetto S, Carrera E, Demasi L. Improved response of unsymmetrically laminated sandwich plates by using zig-zag functions Journal of Sandwich Structures and Materials. 11: 257-267. DOI: 10.1177/1099636208099379  0.474
2009 Demasi L, Yu W. Assess the accuracy of the Variational Asymptotic Plate and Shell Analysis (VAPAS) using the Generalized Unified Formulation (GUF) Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.1080/15376494.2011.584150  0.501
2009 Demasi L, Livne E. Aeroelastic coupling of geometrically nonlinear structures and linear unsteady aerodynamics: Two formulations Journal of Fluids and Structures. 25: 918-935. DOI: 10.1016/J.Jfluidstructs.2009.03.001  0.434
2009 Brischetto S, Carrera E, Demasi L. Improved bending analysis of sandwich plates using a zig-zag function Composite Structures. 89: 408-415. DOI: 10.1016/J.Compstruct.2008.09.001  0.467
2009 Demasi L. ∞6 Mixed plate theories based on the Generalized Unified Formulation. Part I: Governing equations Composite Structures. 87: 1-11. DOI: 10.1016/J.Compstruct.2008.07.013  0.528
2009 Demasi L. ∞6 Mixed plate theories based on the Generalized Unified Formulation. Part II: Layerwise theories Composite Structures. 87: 12-22. DOI: 10.1016/J.Compstruct.2008.07.012  0.506
2009 Demasi L. ∞6 Mixed plate theories based on the Generalized Unified Formulation. Part III: Advanced mixed high order shear deformation theories Composite Structures. 87: 183-194. DOI: 10.1016/J.Compstruct.2008.07.011  0.486
2009 Demasi L. ∞6 Mixed plate theories based on the Generalized Unified Formulation. Part IV: Zig-zag theories Composite Structures. 87: 195-205. DOI: 10.1016/J.Compstruct.2008.07.010  0.488
2009 Demasi L. ∞6 Mixed plate theories based on the Generalized Unified Formulation. Part V: Results Composite Structures. 88: 1-16. DOI: 10.1016/J.Compstruct.2008.07.009  0.514
2009 Demasi L. An invariant model for any composite plate theory and FEM applications: The Generalized Unified Formulation Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.357
2008 Demasi L. 2D, quasi 3D and 3D exact solutions for bending of thick and thin sandwich plates Journal of Sandwich Structures and Materials. 10: 271-310. DOI: 10.1177/1099636208089311  0.504
2008 Demasi L. ∞3 Hierarchy plate theories for thick and thin composite plates: The generalized unified formulation Composite Structures. 84: 256-270. DOI: 10.1016/J.Compstruct.2007.08.004  0.488
2008 Demasi L, Livne E. Dynamic aeroelasticity coupling full order geometrically nonlinear structures and full order linear unsteady aerodynamics - The joined wing case Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference.  0.309
2007 Demasi L, Livne E. Dynamic aeroelasticity of structurally nonlinear configurations using linear modally reduced aerodynamic generalized forces Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 5: 4754-4795. DOI: 10.2514/1.34797  0.42
2007 Demasi L. Investigation on conditions of minimum induced drag of closed wing systems and C-wings Journal of Aircraft. 44: 81-99. DOI: 10.2514/1.21884  0.399
2007 Demasi L. Three-dimensional closed form solutions and exact thin plate theories for isotropic plates Composite Structures. 80: 183-195. DOI: 10.1016/J.Compstruct.2006.04.073  0.478
2007 Demasi L, Livne E. The structural order reduction challenge in the case of geometrically nonlinear joined-wing configurations Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 5: 4274-4293.  0.317
2006 Demasi L, Livne E. Structural Ritz-based simple-polynomial nonlinear equivalent plate approach: An assessment Journal of Aircraft. 43: 1685-1697. DOI: 10.2514/1.17466  0.456
2006 Demasi L. Induced drag minimization: A variational approach using the acceleration potential Journal of Aircraft. 43: 669-680. DOI: 10.2514/1.15982  0.44
2006 Demasi L. Quasi-3D analysis of free vibration of anisotropic plates Composite Structures. 74: 449-457. DOI: 10.1016/J.Compstruct.2005.04.025  0.463
2006 Demasi L. Treatment of stress variables in advanced multilayered plate elements based upon Reissner's mixed variational theorem Computers and Structures. 84: 1215-1221. DOI: 10.1016/J.Compstruc.2006.01.036  0.434
2006 Demasi L, Livne E. Aeroelasticity of structurally nonlinear lifting surfaces using linear modally reduced aerodynamic generalized forces Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 1: 469-487.  0.328
2005 Demasi L. Refined multilayered plate elements based on Murakami zig-zag functions Composite Structures. 70: 308-316. DOI: 10.1016/J.Compstruct.2004.08.036  0.544
2005 Demasi L, Livne E. Exploratory studies of joined wing aeroelasticity Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 7: 4609-4645.  0.317
2005 Demasi L, Livne E. Structural ritz-based simple-polynomial nonlinear equivalent plate approach - An assessment Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 6: 3594-3638.  0.373
2003 Carrera E, Demasi L. Two benchmarks to assess two-dimensional theories of sandwich, composite plates Aiaa Journal. 41: 1356-1362. DOI: 10.2514/2.2081  0.533
2002 Carrera E, Demasi L, Manganello M. Assessment of plate elements on bending and vibrations of composite structures Mechanics of Advanced Materials and Structures. 9: 333-357. DOI: 10.1080/15376490290096982  0.466
2002 Carrera E, Demasi L. Classical and advanced multilayered plate elements based upon PVD and RMVT. Part 2: Numerical implementations International Journal For Numerical Methods in Engineering. 55: 253-291. DOI: 10.1002/Nme.493  0.511
2002 Carrera E, Demasi L. Classical and advanced multilayered plate elements based upon PVD and RMVT. Part 1: Derivation of finite element matrices International Journal For Numerical Methods in Engineering. 55: 191-231. DOI: 10.1002/Nme.492  0.472
1970 Carrera E, Demasi L. An Assessment Of Multilayered Finite PlateElements In View Of The FulfillmentOf The C-Requirements Wit Transactions On Engineering Sciences. 28. DOI: 10.2495/Cp000161  0.496
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