Pretest predictions of the dynamic characteristics of the XV-15 tilting proprotor aircraft are presented. The data for the aircraft in flight include: trim conditions, flight dynamics, gust response, aeroelastic stability and the wing response to control. The data for the aircraft in the Ames 40- by 80-ft wind tunnel include aeroelastic stability and the wing response to control. The calculations were made for pylon tilt angles of 0 deg (airplane mode), 0.1 deg (pylon unlocked), 30, 60, and 90 deg (helicopter mode). (Author)
Predicted Dynamic Characteristics of the XV-15 Tilting Proprotor Aircraft in Flight and in the 40- by 80-Ft. Wind Tunnel
1976
60 pages
Report
Keine Angabe
Englisch
Dynamics of tilting proprotor aircraft in cruise flight
NTRS | 1974
|Dynamics of tilting proprotor aircraft in cruise flight
TIBKAT | 1974
|Dynamics of Tilting Proprotor Aircraft in Cruise Flight
NTIS | 1974
|