Author:
Bogdanski S.,Gansel P.,Lutz T.,Krämer E.
Publisher
Springer International Publishing
Reference11 articles.
1. Pätzold, M.: Auslegungsstudien von 3-D Shock-Control-Bumps mittels numerischer Optimierung (Design of 3D shock control bumps by numerical optimisation), PhD Thesis, Institute for Aerodynamics and Gas Dynamics, University of Stuttgart (2009)
2. Corre, C., et al.: Transonic flow control using a NS-solver and a multi-objective genetic algorithm. Fluid Mech. Appl., 73, 297–302 (2003)
3. Eastwood, J.P., Jarrett, J.P.: Towards designing with three-dimensional bumps for lift/drag improvement and buffet alleviation. AIAA J. 50(12), 2882–2898 (2012)
4. Streit, T., Horstmann, K.-H., Schrauf, G., Hein, S., Fey, U., Egami, Y., Perraud, J., El Din, I., Cella, U., Quest, J.: Complementary numerical and experimental data analysis of the ETW Telfona Pathfinder wing transition tests. 49th AIAA Aerospace Sciences Meeting, Orlando, AIAA Paper 2011-881 (2011)
5. Gerhold, T.: Overview of the Hybrid RANS Code TAU. In: Kroll, N., Fassbender, J.K. (eds.) MEGAFLOW – Numerical Flow Simulation for Aircraft Design. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol. 89, pp. 81–92. Springer, Berlin/Heidelberg (2005)
Cited by
5 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献