Stefanovic, M., and Livne, E., “On the Structural Design Synthesis of Aircraft Engine Pylons at a Certification Level of Detail”, submitted for publication, Journal of Aircraft. In review.

Livne, E, “Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs”, Journal of Aircraft, Vol. 55, No. 1, Jan.-Feb. 2018, pp. 410-452, doi: 10.2514/1.C034442, (41 pages)

Wu, S., and Livne, E., “Alternative Aerodynamic Uncertainty Modeling Approaches for Flutter Reliability Analysis”, AIAA Journal, 2017, Vol.55, pp. 2808-2823, doi: 10.2514/1.J055334

Liu, Y., Bai, J., and Livne, E., “Robust Optimization of Variable-Camber Continuous Trailing-Edge Flap Static Aeroelastic Action”, AIAA Journal, 2017, Vol.55, pp. 1031-1043, doi: 10.2514/1.J055054

Wu, S., and Livne, E., “Probabilistic Aeroservoelastic Reliability Assessment Considering Control System  Component Uncertainty”, AIAA Journal, 2016, Vol.54, pp. 2507-2520, doi: 10.2514/1.J054824 

Chen, P.C., Zhang, Z., and Livne, E., “Design Oriented Computational Fluid Dynamics Based Unsteady  Aerodynamics for Flight Vehicle Shape Optimization”, AIAA Journal, 2015, Vol. 53, No. 12, pp. 3603-3619. doi:  10.2514/1.J054024. 

Jackson, T., and Livne, E., “Integrated Aeroservoelastic Design Optimization of Actively-Controlled Strain Actuated Flight Vehicles”, AIAA Journal, 2014, volume 52, No. 6, pp. 1105-1123, doi: 10.2514/1.J050941 

Styuart, A., Livne, E., Demasi, L., and Mor, M., “Flutter Risk Assessment for Damage Tolerant Composite  Aircraft Structures”, AIAA Journal, Vol. 49, No. 3, March 2011, pp. 655-669.

Bhatia, M., and Livne, E., “Design-Oriented Thermostructural Analysis with External & Internal Radiation. Part  2: Transient Response”, AIAA Journal, 2009, vol. 47, May, No. 5, pp. 1228-1240. 

Demasi, L., and Livne, E., “Aeroelastic Coupling of Geometrically Nonlinear Structures and Linear Unsteady  Aerodynamics: Two Formulations”, Journal of Fluids and Structures, Volume 25, Issue 5, July 2009, Pages 918- 935.

Demasi, L., and Livne, E., “Dynamic Aeroelasticity of Structurally Nonlinear Configurations Using Linear  Modally Reduced Aerodynamic Generalized Forces”, AIAA Journal, 2009, Vol. 47, No.1, pp. 70-90. 

Bhatia, M., and Livne, E., “Shape Sensitivities of Thermoelastic Structures with Internal and External Radiation,  Part I – Steady State”, AIAA Journal, 2008, Vol. 46, No. 3, pp. 578-590.

Mor, M., and Livne, E., “Shape Sensitivities Of Minimum-State Unsteady Aerodynamics Approximations using  Sensitivity of Optimal Solutions to Problem Parameters”, AIAA Journal, 2007, Vol. 45, No. 9, pp. 2187-2195. 

Mor, M., and Livne, E., “Sensitivities and Approximations for Aeroservoelastic Shape Optimization with Gust  Response Constraints”, Journal of Aircraft, 2006, vol.43 no.5, pp. 1516-1527.

Demasi, L., and Livne, E., “Structural Ritz-Based Simple-Polynomial Nonlinear Equivalent Plate Approach: An  Assessment”, Journal of Aircraft, 2006, vol.43, no.6, pp. 1685-1697

Livne, E., and Coskuner, L., “Design-Oriented Structural-Acoustic Reduced-Order Frequency Response:  Combined Direct / Adjoint Approximations”, AIAA Journal, 2006, Vol. 44, No. 8, pp. 1835-1844. 

Chen, P.C., Liu, D.D., and Livne, E., “Unsteady Aerodynamic Shape Sensitivities for Airplane Aeroservoelastic  Configuration Optimization”,Journal of Aircraft, vol.43, no.2, 2006, pp. 471-481. 

Jackson, T., and Livne, E., “Design-Oriented Structural Model Order Reduction for Strain-Actuated Flight  Vehicle Structures”, AIAA Journal of Aircraft, Journal of Aircraft, vol.43, no.1, 2006, pp. 182-188. 

Mor, M., and Livne, E., “Minimum-State Unsteady Aerodynamics for Aeroservoelastic Configuration Shape  Optimization of Flight Vehicles”, AIAA Journal, Vol. 43, No. 11, November 2005, pp. 2299-2308. 

Engelsen, F., and Livne, E., “A Design-oriented Mode Acceleration Method for Lyapunov’s Equation Based  Random Gust Stresses in Aeroservoelastic Optimization”, Journal of Aircraft, Vol. 41, No. 2, March-April 2004,  pp. 335-347. 

Engelsen, F., and Livne, E., “Quadratic Stress Failure Constraints for Structures under Combined Steady and  Random Excitation”, AIAA Journal, Vol. 42, No. 1, January 2004, pp. 132-140. 

Livne, E., “Future of Airplane Aeroelasticity”, Journal of Aircraft, Vol. 40, No. 6, November-December 2003, pp.  1066-1092. 

Livne, E., and Weisshaar, T.A., “Aeroelasticity of Nonconventional Airplane Configurations – Past and Future”,  Journal of Aircraft, Vol. 40, No. 6, November-December 2003, pp. 1047-1065.

Livne, E., and Blando, G.D., “Structural Dynamics Frequency Response Using Combined Direct and  Adjoint Reduced-Order Approximations”, AIAA Journal, Vol. 41, No. 7, July 2003, pp. 1377-1385.

Livne, E., and Blando, G.D., “Design-Oriented static and dynamic Stress Analysis Using Combined Direct  and Adjoint Reduced Order Solutions”, AIAA Journal, Vol. 38, No. 5, May 2000, pp. 898-909.