Aerodynamic Design Optimization of Three Dimensional Rocket Nozzles Using Adjoint Method
21st AIAA Computational Fluid Dynamics Conference
01.01.2013
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Three-Dimensional Aerodynamic Design Optimization of a Turbine Blade by Using an Adjoint Method
Online Contents | 2011
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