Title :
Effects of terminal voltage, load current, and minimum rotor speed on the weight of D-C aircraft generators
Author_Institution :
Naval Research Laboratory, Washington, D. C.
Abstract :
THE weight of aircraft electric power systems is of major importance because unnecessary weight carried in an airplane reduces the pay load.
Keywords :
Aircraft; Cooling; Equations; Generators; Mathematical model; Temperature measurement; Windings;
Journal_Title :
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
DOI :
10.1109/TAI.1952.6371224
