Longitudinal and lateral stability and control characteristics were investigated from hovering to forward flight; tests covered pure tilt wing, tilt wing with flap, slats, wing span extension, and tilt wing with speed brakes and slats; tests were conducted in and out of ground effect and included investigation of stabilizer and tail fan effectiveness.
Aerodynamic characteristics of four-propeller tilt-wing VTOL model with twin vertical tails, including effects of ground proximity
NASA -- Tech Note
1961
137 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1960
|