Aerodynamic characteristics of tilt-wing and deflected slip-stream configurations are examined; it appears that for propeller driven VTO L aircraft, combination of 2 principles (tilt-wing and flap configuration) should be used.
Aerodynamic characteristics of propeller-driven VTOL aircraft
NASA -- Tech Note
1961
16 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
INVESTIGATION ON AERODYNAMIC DESIGN OF VTOL AIRCRAFT PROPELLER
DataCite | 2024
|Field requirements of overloaded propeller-driven VTOL aircraft
Engineering Index Backfile | 1963
|