The theory of governing for aircraft turbo alternators
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 January 1972
Abstract
The first part of this feature which appeared last month, covered dynamics of the throttle, the electro‐hydraulic governor, governor internal loop stability and alternative methods of stabilisation.
Citation
BURNS, D.O. (1972), "The theory of governing for aircraft turbo alternators", Aircraft Engineering and Aerospace Technology, Vol. 44 No. 1, pp. 20-22. https://doi.org/10.1108/eb034855
Publisher
:MCB UP Ltd
Copyright © 1972, MCB UP Limited