Investigation in Langley full scale tunnel of stability and control characteristics of convertible type airplane (combination helicopter and airplane) for normal flight attitudes with full power and also for high angles of attack including transition to hovering attitude; comparisons of effects of articulated and rigid propeller operation.
Static longitudinal stability and control of convertible-type airplane as affected by articulated- and rigid-propeller operation
Nat Advisory Committee Aeronautics -- Tech Note
1950
49 pages
Report
English
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Propeller thrust force contribution to airplane longitudinal stability
Emerald Group Publishing | 2018
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