Application of a Weighted Average Surrogate Approach to Helicopter Rotor Blade Vibration Reduction
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; 2007 ; Honolulu , Hawaii
01.01.2007
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Multiple-surrogate approach to helicopter rotor blade vibration reduction
Tema Archiv | 2009
|Multiple-Surrogate Approach to Helicopter Rotor Blade Vibration Reduction
Online Contents | 2009
|British Library Conference Proceedings | 2007
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