Three Dimensional Direct Turbine Blade Design Method
32nd AIAA Fluid Dynamics Conference and Exhibit ; 2002 ; St. Louis , Missouri
01.01.2002
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A parametric method for direct gas-turbine-blade design
AIAA | 1987
|Three-Dimensional Aerodynamic Design Optimization of a Turbine Blade by Using an Adjoint Method
Online Contents | 2011
|Three-Dimensional Boundary Layer in a Turbine Blade Passage
Online Contents | 2017
|Three-Dimensional Boundary Layer in a Turbine Blade Passage
Online Contents | 2017
|