| Future of airplane aeroelasticity E Livne Journal of Aircraft 40 (6), 1066-1092, 2003 | 241 | 2003 |
| Aircraft active flutter suppression: State of the art and technology maturation needs E Livne Journal of Aircraft 55 (1), 410-452, 2018 | 227 | 2018 |
| Aeroelasticity of nonconventional airplane configurations-past and future E Livne, TA Weisshaar Journal of Aircraft 40 (6), 1047-1065, 2003 | 163 | 2003 |
| Integrated aeroservoelastic optimization: status and direction E Livne Journal of Aircraft 36 (1), 122-145, 1999 | 161 | 1999 |
| Aeroelasticity of joined-wing airplane configurations-Past work and future challenges-a survey E Livne 19th AIAA Applied Aerodynamics Conference, 1370, 2001 | 74 | 2001 |
| Integrated structure/control/aerodynamic synthesis of actively controlled composite wings E Livne, LA Schmit, PP Friedmann Journal of Aircraft 30 (3), 387-394, 1993 | 57 | 1993 |
| Dynamic aeroelasticity of structurally nonlinear configurations using linear modally reduced aerodynamic generalized forces L Demasi, E Livne AIAA journal 47 (1), 70-90, 2009 | 55 | 2009 |
| Equivalent plate structural modeling for wing shape optimization including transverse shear E Livne AIAA journal 32 (6), 1278-1288, 1994 | 54 | 1994 |
| Towards integrated multidisciplinary synthesis of actively controlled fiber composite wings E Livne, LA Schmit, PP Friedmann Journal of Aircraft 27 (12), 979-992, 1990 | 46 | 1990 |
| Nonlinear equivalent plate modeling of wing-box structures E Livne, I Navarro Journal of Aircraft 36 (5), 851-865, 1999 | 40 | 1999 |
| Experimental investigation of a flexible wing with a variable camber continuous trailing edge flap design NT Nguyen, E Livne, N Precup, JM Urnes, C Nelson, E Ting, S Lebofsky 32nd AIAA Applied Aerodynamics Conference, 2441, 2014 | 39 | 2014 |
| Lessons from application of equivalent plate structural molding to an HSCT wing E Livne, RA Sels, KG Bhatia Journal of aircraft 31 (4), 953-960, 1994 | 39 | 1994 |
| Aeroelastic coupling of geometrically nonlinear structures and linear unsteady aerodynamics: two formulations L Demasi, E Livne Journal of Fluids and Structures 25 (5), 918-935, 2009 | 36 | 2009 |
| Aeroservoelastic aspects of wing/control surface planform shape optimization E Livne, WL Li AIAA journal 33 (2), 302-311, 1995 | 32 | 1995 |
| Alternative approximations for integrated control/structure aeroservoelastic synthesis E Livne AIAA journal 31 (6), 1100-1108, 1993 | 31 | 1993 |
| Wind tunnel investigation of a flexible wing high-lift configuration with a variable camber continuous trailing edge flap design NT Nguyen, N Precup, E Livne, JM Urnes, E Dickey, C Nelson, J Chiew, ... 33rd AIAA Applied Aerodynamics Conference, 2417, 2015 | 26 | 2015 |
| Design, construction, and tests of an aeroelastic wind tunnel model of a variable camber continuous trailing edge flap (vcctef) concept wing E Livne, N Precup, M Mor 32nd AIAA Applied Aerodynamics Conference, 2442, 2014 | 26 | 2014 |
| Exploratory Studies of Joined-Wing Aeroelasticity L Demasi, E Livne 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2005 | 26 | 2005 |
| Accurate calculation of control-augmented structural eigenvalue sensitivities using reduced-order models E Livne AIAA journal 27 (7), 947-954, 1989 | 26 | 1989 |
| Integrated aeroservoelastic design optimization of actively controlled strain-actuated flight vehicles T Jackson, E Livne AIAA journal 52 (6), 1105-1123, 2014 | 25 | 2014 |
