With increasing use of four-engined transport and bomber it has become necessary to develop means to reduce physical effort required to operate flight controls; prerequisites of booster control system summarized; methods which now offer solution to problem.
Surface control booster for large aircraft
Aero Digest
Aero Digest ; 37 , n 2 ; p 76 + 80
1940
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Reliability Analysis for the Hydraulic Booster Control Surface of Aircraft
Online Contents | 2017
|Reliability Analysis for the Hydraulic Booster Control Surface of Aircraft
Online Contents | 2017
|