It is shown that wing stall can be encountered even though entire wing is immersed in propeller slipstream; effects of wing stall on power requirements in transition speed range and on take off and landing distance; with stall under control, STOL performance becomes primarily function of amount of power installed in airplane.
Take-off and landing distance and power requirements of propeller-driven STOL airplanes
Aeronautical Eng Rev
Aeronautical Engineering Review ; 16 , n 11
1957
5 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Ducted propeller for STOL airplanes
Engineering Index Backfile | 1960
|Problems in design of propeller-driven vertical take-off transport airplanes
Engineering Index Backfile | 1956
|Feature for Distinguishing Propeller-Driven Airplanes from Turbine-Driven Airplanes
Online Contents | 2010
|Introduction to V/STOL airplanes
TIBKAT | 1981
|