DocumentCode
1370042
Title
Effects of terminal voltage, load current, and minimum rotor speed on the weight of D-C aircraft generators
Author
Scott, H. Dale
Author_Institution
Naval Research Laboratory, Washington, D. C.
Volume
71
Issue
4
fYear
1952
Firstpage
191
Lastpage
197
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;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
Publisher
ieee
ISSN
0097-2185
Type
jour
DOI
10.1109/TAI.1952.6371224
Filename
6371224
Link To Document