DLR transonic inverse design code, extensions and modifications to increase versatility and robustness
暂无分享,去创建一个
[1] W. Heinze,et al. Three Surface Aircraft - A Concept For Future Transport Aircraft , 2000 .
[2] David W. Zingg,et al. Optimization of Subsonic and Transonic Airfoils for Natural Laminar Flow using a Discrete-Adjoint Method , 2015 .
[3] Thomas Streit,et al. Erweiterung des 3D inversen Verfahrens auf Randbedingungen mit 2 Symmetrieebenen , 2016 .
[4] Caslav Ilic,et al. Towards cooperative high-fidelity aircraft MDO: comparison of Breguet and ODE evaluation of the cruise mission segment , 2014 .
[5] Stefan Görtz,et al. AN EFFICIENT AERODYNAMIC SHAPE OPTIMIZATION FRAMEWORK FOR ROBUST DESIGN OF AIRFOILS USING SURROGATE MODELS , 2016 .
[6] Jens K. Fassbender,et al. MEGAFLOW - Numerical Flow Simulation for Aircraft Design , 2005 .
[7] Richard L. Campbell,et al. Progress Toward Efficient Laminar Flow Analysis and Design , 2011 .
[8] Thomas Streit,et al. Aerodynamic Design Study for Multi-Lifting Surfaces , 2005 .
[9] M. Hepperle,et al. Application of an Inverse Design Method to the Design of Transonic Nacelles , 1996 .
[10] Stefan Görtz,et al. Efficient Global Optimization of a Natural Laminar Airfoil Based on Surrogate Modeling , 2014 .
[11] Wolf Bartelheimer,et al. An inverse method for the design of transonic airfoils and wings , 1996 .
[12] Kisa Matsushima,et al. An Inverse Design Method for Wings Using Integral Equations and Its Recent Progress , 1999 .
[13] Thomas Streit,et al. DLR natural and hybrid transonic laminar wing design incorporating new methodologies , 2015, The Aeronautical Journal.
[14] Mohammad Abu-Zurayk,et al. Aero-Elastic Multipoint Optimization Using the Coupled Adjoint Approach , 2014 .
[15] Richard L. Campbell,et al. Efficient Viscous Design of Realistic Aircraft Configurations , 1998 .
[16] Kazuhiro Nakahashi,et al. Wing design for supersonic transports using integral equation method , 2004 .
[17] S. Takanashi,et al. Iterative three-dimensional transonic wing design using integral equations , 1985 .
[18] Tobias Bach,et al. Entwicklung einer Softwareplattform für die Multidisziplinäre Optimierung eines Gesamtflugzeugs , 2014 .
[19] W. Bartelheimer. Ein Entwurfsverfahren für Tragflügel in transsonischer Strömung , 1996 .
[20] T. Streit,et al. THREE-SURFACE AIRCRAFT - A CONCEPT FOR FUTURE LARGE AIRCRAFT , 2000 .
[21] Thomas Gerhold,et al. Overview of the Hybrid RANS Code TAU , 2005 .
[22] L. Richard,et al. An Approach to Constrained Aerodynamic Design With Application to Airfoils , 2003 .
[23] G. Krenz. Transonic wing design for transport aircraft , 1979 .
[24] S. Obayashi,et al. Genetic optimization of target pressure distributions for inverse design methods , 1996 .
[25] Z. Mengmeng,et al. Transonic Airfoil and Wing Design Using Inverse and Direct Methods , 2015 .
[26] Mohammad Abu-Zurayk,et al. Aerodynamic Inverse Design Framework Using Discrete Adjoint Method , 2013 .