The aerodynamic configuration of a vertical takeoff transport aircraft with fan lift propulsion system is discussed. Specifications of the geometry, inertia, and aerodynamic characteristics are presented. The composition and performance of the propulsion system are analyzed. Tables of data are included to show dimensions and predicted performance.
Aircraft Design Studies Vertical Take off and Landing Airliner
1972
53 pages
Report
No indication
English
Design method of vertical take-off and landing aircraft and vertical take-off and landing aircraft
European Patent Office | 2024
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