Stability and control systems adopted by Bell Aircraft Corp and for Short S.C.1 are discussed with regard to efficiency; importance of low loss nozzle systems; form of auto stabilization and its application to aircraft control system are governed by operating requirements of VTOL aircraft; lift engine intake problems and interaction effects of airflow passing through lift engines on airframe are considered; ground effects and novel model testing techniques, future research needed.
Aerodynamic design problems of jet lift V.T.O.L. Aircraft
Aircraft Eng
Aircraft Engineering ; 34 , n 401
1962
4 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Prospects for civil V.T.O.L. Aircraft
Engineering Index Backfile | 1966
|The Prospects for Civil V.T.O.L. Aircraft
Emerald Group Publishing | 1966
|Aerodynamic Design Problems of Jet Lift V.T.O.L Aircraft
Emerald Group Publishing | 1962
|Aerodynamic Problems of high lift
TIBKAT | 1962
|