The theory of governing for aircraft turbo alternators

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