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 :
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