EFFECTS OF ROTOR BLADE TORSIONAL FLEXIBILITY IN HOVERING FLIGHT Document Details Document Type Technical Report Publication Date Dec 31, 1955 Accession Number AD0091235 Entities People Paul Warsett Organizations Honeywell International, Inc. Tags DTIC Thesaurus Topics Aircrafts Automatic Control Systems Flight Flight Maneuvers Helicopters Hovering Mechanical Properties Physical Properties Resilience