DocumentCode
1346521
Title
Ten years of progress in predicting the aerodynamic, thermodynamic, and output characteristics of blast-cooled aircraft generators
Author
Scott, D. H.
Author_Institution
Naval Research Laboratory, Washington, D. C.
Volume
73
Issue
6
fYear
1955
Firstpage
455
Lastpage
461
Abstract
THE output of electric apparatus is limited usually by maximum allowable temperatures. If electromagnetic and other design factors permit, the output can be increased by applying additional cooling. This increased cooling principle permits greater output per pound of electric apparatus and has been applied to aircraft generators for a number of years to increase electric system capacity and reduce installed weight.
Keywords
Aircraft; Cooling; Equations; Generators; Heat transfer; Heating; Wires;
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.1955.6367098
Filename
6367098
Link To Document