Existing and proposed VTOL test beds examined and their characteristics compared with helicopter requirements on basis of angular acceleration and velocity capability in pitch, roll and yaw; it is found that stability and control requirements of helicopters are applicable; tentative hovering and transition flying qualities for VTOL aircraft should be established using same criteria contained in helicopter specification MIL-H-8501.
Hovering and low speed controllability of VTOL aircraft
Am Helicopter Soc -- J
American Helicopter Society -- Journal ; 4 , n 1
1959
3 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Thrust losses in hovering for jet VTOL AIRCRAFT
NTRS | 1966
|Effect of stabilization on VTOL aircraft in Hovering flight
TIBKAT | 1972
|