☰

Melike Nikbay, Ph.D. - Publications

Affiliations: 
2002 University of Colorado, Boulder, Boulder, CO, United States 
Area:
Aerospace Engineering, Applied Mechanics, Mechanical Engineering
Tree Info Similar researchers PubMed Report error

24 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
2018 Tola C, Nikbay M. Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach Journal of Spacecraft and Rockets. 55: 936-947. DOI: 10.2514/1.A34066  0.397
2018 Tola C, Nikbay M. Solid rocket motor design using a surrogate model Aircraft Engineering and Aerospace Technology. 90: 1104-1127. DOI: 10.1108/Aeat-01-2017-0045  0.369
2016 Nikbay M, Acar P. Aeroelastic predictions for steady and unsteady flow characteristics of the HIRENASD wing Progress in Computational Fluid Dynamics. 16: 26-37. DOI: 10.1504/Pcfd.2016.074253  0.464
2015 Nikbay M, Acar P, Aslan AR. Development of a nanosatellite de-orbiting system by reliability based design optimization Acta Astronautica. 117: 469-483. DOI: 10.1016/J.Actaastro.2015.09.002  0.444
2015 Nikbay M, Acar P. Reduced order modelling for static and dynamic aeroelastic predictions with multidisciplinary approach Ceas Aeronautical Journal. 6: 455-469. DOI: 10.1007/S13272-015-0154-3  0.402
2015 Nikbay M, Acar P. Multidisciplinary uncertainty quantification in aeroelastic analyses of semi-span supersonic transport wing 16th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference.  0.307
2014 Nikbay M, Fakkusoglu N, Kuru MN. Reliability-based aeroelastic optimization of a composite aircraft wing via fluid-structure interaction of high fidelity solvers Iop Conference Series: Materials Science and Engineering. 10. DOI: 10.1088/1757-899X/10/1/012037  0.482
2013 Acar P, Nikbay M. Steady and unsteady aeroelastic computations of HIRENASD wing for low and high Reynolds numbers Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. DOI: 10.2514/6.2013-1800  0.362
2013 Nikbay M, Kuru MN. Reliability based multidisciplinary optimization of aeroelastic systems with structural and aerodynamic uncertainties Journal of Aircraft. 50: 708-715. DOI: 10.2514/1.C031693  0.545
2012 Nikbay M, Acar P. Robust aeroelastic design optimization of wing/store configurations based on flutter criteria 12th Aiaa Aviation Technology, Integration and Operations (Atio) Conference and 14th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference.  0.467
2012 Nikbay M, Acar P, Rüstem Aslan A. Reliability based design optimization of a CubeSat de-orbiting mechanism 12th Aiaa Aviation Technology, Integration and Operations (Atio) Conference and 14th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference.  0.389
2012 Nikbay M, Acar P. Flutter based aeroelastic optimization of an aircraft wing with analytical approach 53rd Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference 2012.  0.41
2010 Nikbay M, Kuru MN, Bayat S, Fakkusoglu N. Reliability-based design optimisation of an aircraft wing structure with high-fidelity modelling International Journal of Design Engineering. 3: 247. DOI: 10.1504/Ijde.2010.039759  0.43
2009 Nikbay M, Öncü L, Aysan A. Multidisciplinary code coupling for analysis and optimization of aeroelastic systems Journal of Aircraft. 46: 1938-1944. DOI: 10.2514/1.41491  0.557
2008 Maute K, Farhat C, Argrow B, Nikbay M. Sonic boom mitigation via shape optimization using an adjoint method and application to a supersonic fighter aircraft European Journal of Computational Mechanics. 17: 217-243. DOI: 10.3166/Remn.17.217-243  0.611
2008 Nikbay M, Öncü L, Aysan A. A multi-disiplinary code coupling approach for analysis and optimization of aeroelastic systems 12th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference, Mao.  0.5
2007 Farhat C, Maute K, Argrow B, Nikbay M. Shape optimization methodology for reducing the sonic boom initial pressure rise Aiaa Journal. 45: 1007-1018. DOI: 10.2514/1.27607  0.585
2004 Farhat C, Argrow B, Nikbay M, Maute K. Shape Optimization with F-Function Balancing for Reducing the Sonic Boom Initial Shock Pressure Rise International Journal of Aeroacoustics. 3: 361-377. DOI: 10.1260/1475472043499281  0.628
2003 Argrow B, Farhat C, Maute K, Nikbay M. Linear-theory-based shape optimization for sonic boom minimization Fluid Mechanics and Its Applications. 73: 349-354. DOI: 10.1007/978-94-010-0017-8_52  0.579
2003 Maute K, Nikbay M, Farhat C. Sensitivity analysis and design optimization of three-dimensional non-linear aeroelastic systems by the adjoint method International Journal For Numerical Methods in Engineering. 56: 911-933. DOI: 10.1002/Nme.599  0.627
2002 Farhat C, Maute K, Argrow B, Nikbay M. A shape optimization methodology for reducing the sonic boom initial pressure rise 40th Aiaa Aerospace Sciences Meeting and Exhibit. DOI: 10.2514/1.27607  0.649
2002 Farhat C, Argrow B, Nikbay M, Maute K. A shape optimization methodology with F-function lobe balancing for mitigating the sonic boom 9th Aiaa/Issmo Symposium On Multidisciplinary Analysis and Optimization.  0.61
2001 Maute K, Nikbay M, Farhat C. Coupled analytical sensitivity analysis and optimization of three-dimensional nonlinear aeroelastic systems Aiaa Journal. 39: 2051-2061. DOI: 10.2514/2.1227  0.64
2000 Maute K, Nikbay M, Farhat C. Analytically based sensitivity analysis and optimization of nonlinear aeroelastic systems 8th Symposium On Multidisciplinary Analysis and Optimization.  0.623
Show low-probability matches.