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- W1036246581 abstract "Composite structures technology is applied in a preliminary design study of advanced technology blades and hubs for the XV-15 tilt rotor research demonstrator aircraft. Significant improvements in XV-15 hover and cruise performance are available using blades designed for compatibility with the existing aircraft, i.e., blade installation would not require modification of the airframe, hub or upper controls. Provision of a low risk nonmechanical control system was also studied, and a development specification is given." @default.
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- W1036246581 date "1979-11-01" @default.
- W1036246581 modified "2023-09-27" @default.
- W1036246581 title "Preliminary design study of advanced composite blade and hub and nonmechanical control system for the tilt-rotor aircraft. Volume 1: Engineering studies" @default.
- W1036246581 hasPublicationYear "1979" @default.
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