Some Design Considerations for a Hydraulic Servo: A Treatment of a Type in which the two‐stage Control Valve has a Flapper‐Nozzle Valve as its First Stage
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 August 1956
Abstract
PROMINENT among hydraulic servos today are those being developed in the aeronautical field, both for conventional aircraft and for guided missiles. In general these applications demand the following characteristics of the servos:
Citation
Nightingale, J.M. (1956), "Some Design Considerations for a Hydraulic Servo: A Treatment of a Type in which the two‐stage Control Valve has a Flapper‐Nozzle Valve as its First Stage", Aircraft Engineering and Aerospace Technology, Vol. 28 No. 8, pp. 254-258. https://doi.org/10.1108/eb032721
Publisher
:MCB UP Ltd
Copyright © 1956, MCB UP Limited