Return to search

Helicopter Vibration Reduction Using Single Crystal And Soft Piezoceramic Shear Induced Active Blade Twist

No description available.
Identiferoai:union.ndltd.org:IISc/oai:etd.ncsi.iisc.ernet.in:2005/1477
Date04 1900
CreatorsThakkar, Dipali
ContributorsGanguli, Ranjan
Source SetsIndia Institute of Science
Languageen_US
Detected LanguageEnglish
TypeThesis
RelationG19167

Page generated in 0.0021 seconds