Investigation of a Helicopter Individual Blade Control (IBC) System in Two Full-Scale Wind Tunnel Tests: Volume I

This report presents the data acquired during the testing of an individual blade control (IBC) system on a full-scale helicopter rotor in two test entries in the NASA Ames 40- by 80-Foot Wind Tunnel. The objective of these investigations was to evaluate the potential benefits of using IBC to improve...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Jacklin, Stephen A, Swanson, Stephen, Blaas, Achim, Teves, Dietrich, Niesl, Georg, Kube, Roland, Key, David L, Gmelin, Bernd
Format:	Report
Sprache:	eng
Schlagworte:	Aeronautics (General)
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