Aerodynamic Design Optimization of Helicopter Rotor Blades in Hover Performance Using Advanced Configuration Generation Method
35th, European rotorcraft forum ; 2009 ; Hamburg, Germany
01.01.2009
1177 pages
Held on CD-ROM; Held in e-store (RMS)
Aufsatz (Konferenz)
Englisch
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Aerodynamic Shape Optimization of Rotor Blades in Hover Using Unstructured Meshes
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